CHAPTER 21. DUCT DESIGN

 

Commercial, industrial, and residential air duct system design must consider (1) space availability, (2) noise levels, (3) air leakage, (4) balancing, (5) fire and smoke control, (6) initial investment cost, and (7) system operating cost.

Deficiencies in duct design can result in systems that operate incorrectly or are expensive (increased energy) to own and operate. Poor design or lack of system sealing can produce inadequate airflow rates at the terminals, leading to discomfort, loss of productivity, and even adverse health effects. Lack of sound attenuation may lead to objectionable noise levels. Proper duct insulation eliminates excessive heat gain or loss.

In this chapter, system design and calculation of a system’s frictional and dynamic resistance (total pressure) to airflow are considered. Chapter 19 of the 2020 ASHRAE Handbook—HVAC Systems and Equipment examines duct construction and presents construction standards for residential, commercial, and industrial HVAC and exhaust systems. For design guidance specific to residential systems, refer to Manual D by ACCA (2014).

1. BERNOULLI EQUATION

The Bernoulli equation can be developed by equating the forces on an element of a stream tube in a frictionless fluid flow to the rate of momentum change. On integrating this relationship for steady flow, the following expression (Osborne 1966) results:

(1)

where

v = streamline (local) velocity, fps
gc = dimensional constant, 32.2 lbm · ft/lbf · s2
p = absolute pressure, lbf/ft2
ρ = density, lbm/ft3
g = acceleration caused by gravity, ft/s2
z = elevation, ft

Assuming constant fluid density in the system, Equation (1) reduces to

(2)

Although Equation (2) was derived for steady, ideal frictionless flow along a stream tube, it can be extended to analyze flow through ducts in real systems. In terms of pressure, the relationship for fluid resistance between two sections is

(3)

where

V = average duct velocity, fps
Δpt,1–2 = total pressure loss caused by friction and dynamic losses between sections 1 and 2, lbf/ft2

In Equation (3), V (section average velocity) replaces v (streamline velocity) because experimentally determined loss coefficients allow for errors in calculatingv2/2gc (velocity pressure) across streamlines.

On the left side of Equation (3), add and subtract pz1; on the right side, add and subtract pz2, where pz1 and pz2 are the values of atmospheric air at heights z1 and z2. Thus,

(4)

Atmospheric pressure at any elevation (pz1 and pz2) expressed in terms of the atmospheric pressure pa at the same datum elevation is given by

(5)

(6)

Substituting Equations (5) and (6) into Equation (4) and simplifying yields the total pressure change between sections 1 and 2. Assume no temperature change between sections 1 and 2 (no heat exchanger within the section); therefore, ρ1 = ρ2. When a heat exchanger is located in the section, the average of the inlet and outlet temperatures is generally used. Let ρ = ρ1 = ρ2, and (p1pz1) and (p2pz2) are gage pressures at elevations z1 and z2.

(7a)

(7b)

Rearranging Equation (7b) yields

(7c)

where

ps, 1 = static pressure, gage at elevation z1, lbf/ft2
ps, 2 = static pressure, gage at elevation z2, lbf/ft2
V1 = average velocity at section 1, fps
V2 = average velocity at section 2, fps
ρa = density of ambient air, lbm/ft3
ρ = density of air or gas in duct, lbm/ft3
Δpse = thermal gravity effect, lbf/ft2
Δpt = total pressure change between sections 1 and 2, lbf/ft2
Δpt,1–2 = total pressure loss caused by friction and dynamic losses between sections 1 and 2, lbf/ft2

1.1  HEAD AND PRESSURE

The terms head and pressure are often used interchangeably; however, head is the height of a fluid column supported by fluid flow, whereas pressure is the normal force per unit area. For liquids, it is convenient to measure head in terms of the flowing fluid. With a gas or air, however, it is customary to measure pressure exerted by the gas on a column of liquid.

 Static Pressure

The term pgcg is static head; p is static pressure.

 Velocity Pressure

The term V2/2g refers to velocity head, and ρV2/2gc refers to velocity pressure. Although velocity head is independent of fluid density, velocity pressure [Equation (8)] is not.

(8)

where

pv = velocity pressure, in. of water
V = fluid mean velocity, fpm
1097 = conversion factor to in. of water

For air at standard conditions (0.075 lbm/ft3), Equation (8) becomes

(9)

where 4005 = (10972/0.075)1/2. Velocity is calculated by

(10)

where

Q = airflow rate, cfm
A = cross-sectional area of duct, ft2

 Total Pressure

Total pressure is the sum of static pressure and velocity pressure:

(11)

or

(12)

where

pt = total pressure, in. of water
ps = static pressure, in. of water

 Pressure Measurement

The range, precision, and limitations of instruments for measuring pressure and velocity are discussed in Chapter 36. The manometer is a simple and useful means for measuring partial vacuum and low pressure. Static, velocity, and total pressures in a duct system relative to ambient space pressure can be measured with a pitot tube connected to a manometer. Pitot tube construction and locations for traversing round and rectangular ducts are presented in Chapter 37.

2. SYSTEM ANALYSIS

The total pressure change caused by friction, fittings, equipment, and net thermal gravity effect for each section of a duct system is calculated by the following equation:

(13)

where

Δpti = net total pressure change for i sections, in. of water
Δpfi = pressure loss caused by friction for i sections, in. of water
Δpij = total pressure loss caused by j fittings, including fan system effect (FSE), for i sections, in. of water
Δpik = pressure loss caused by k equipment for i sections, in. of water
Δpseir = thermal gravity effect caused by r stacks for i sections, in. of water
m = number of fittings within i sections
n = number of equipment within i sections
λ = number of stacks within i sections
nup = number of duct sections upstream of fan (exhaust/return air subsystems)
ndn = number of duct sections downstream of fan (supply air subsystems)

From Equation (7), the thermal gravity effect for each nonhorizontal duct with a density other than that of ambient air is determined by the following equation:

(14)

where

Δpse = thermal gravity effect, in. of water
z1 and z2 = elevation from datum in direction of airflow (Figure 1), ft
ρa = density of ambient air, lbm/ft3
ρ = density of air or gas within duct, lbm/ft3
0.192 = conversion factor to in. of water

Example 1.

For Figure 1, calculate the thermal gravity effect for two cases: (a) air cooled to −30°F, and (b) air heated to 1000°F. Density of air at −30°F is 0.0924 lbm/ft3 and at 1000°F is 0.0271 lbm/ft3. Density of ambient air is 0.075 lbm/ft3. Stack height is 40 ft.

Solution:

(a) For ρ > ρa (Figure 1A),

(b) For ρ < ρa (Figure 1B),


Example 2.

Calculate the thermal gravity effect for the two-stack system shown in Figure 2, where the air is 250°F and stack heights are 50 and 100 ft. Density of 250°F air is 0.0558 lbm/ft3; ambient air is 0.075 lbm/ft3.

Solution:


For the system shown in Figure 3, the direction of air movement created by the thermal gravity effect depends on the initiating force (e.g., fans, wind, opening and closing doors, turning equipment on and off). If for any reason air starts to enter the left stack (Figure 3A), it creates a buoyancy effect in the right stack. On the other hand, if flow starts to enter the right stack (Figure 3B), it creates a buoyancy effect in the left stack. In both cases, the produced thermal gravity effect is stable and depends on stack height and magnitude of heating. The starting direction of flow is important when using natural convection for ventilation.

To determine the fan total pressure requirement for a system, use the following equation:

(15)

where

Fup and Fdn = sets of duct sections upstream and downstream of fan
Pt = fan total pressure, in. of water
ε = symbol that ties duct sections into system paths from exhaust/return air terminals to supply terminals

Figure 4 shows the use of Equation (15). This system has three supply and two return terminals consisting of nine sections connected in six paths: 1-3-4-9-7-5, 1-3-4-9-7-6, 1-3-4-9-8, 2-4-9-7-5, 2-4-9-7-6, and 2-4-9-8. Sections 1 and 3 are unequal area; thus, they are assigned separate numbers in accordance with the rules for identifying sections (see step 5 in the section on HVAC Duct Design Procedures). To determine the fan pressure requirement, apply the following six equations, derived from Equation (15). These equations must be satisfied to attain pressure balancing for design airflow. Relying entirely on dampers is not economical and may create objectionable flow-generated noise.

(16)

Thermal Gravity Effect for Example 1

Figure 1. Thermal Gravity Effect for Example 1


Multiple Stacks for Example 2

Figure 2. Multiple Stacks for Example 2


Example 3.

For Figures 5A and 5C, calculate the thermal gravity effect and fan total pressure required when the air is cooled to −30°F. The heat exchanger and ductwork (section 1 to 2) total pressure losses are 0.70 and 0.28 in. of water respectively. Density of −30°F air is 0.0924 lbm/ft3; ambient air is 0.075 lbm/ft3. Elevations are 70 and 10 ft.

Solution:

(a) For Figure 5A (downward flow),

(b) For Figure 5C (upward flow),


Multiple Stack Analysis

Figure 3. Multiple Stack Analysis


Illustrative 6-Path, 9-Section System

Figure 4. Illustrative 6-Path, 9-Section System


Single Stack with Fan for Examples 3 and 4

Figure 5. Single Stack with Fan for Examples 3 and 4


Example 4.

For Figures 5B and 5D, calculate the thermal gravity effect and fan total pressure required when air is heated to 250°F. Heat exchanger and ductwork (section 1 to 2) total pressure losses are 0.70 and 0.28 in. of water, respectively. Density of 250°F air is 0.0558 lbm/ft3; ambient air is 0.075 lbm/ft3. Elevations are 70 and 10 ft.

Solution:

(a) For Figure 5B (downward flow),

(b) For Figure 5D (upward flow),

Example 5.

Calculate the thermal gravity effect for each section of the system in Figure 6 and the system’s net thermal gravity effect. Density of ambient air is 0.075 lbm/ft3, and the lengths are as follows: z1 = 50 ft, z2 = 90 ft, z4 = 95 ft, z5 = 25 ft, and z9 = 200 ft. Pressure required at section 3 is −0.1 in. of water. Write the equation to determine the fan total pressure requirement.

Solution: The following table summarizes the thermal gravity effect for each section of the system as calculated by Equation (14). The net thermal gravity effect for the system is 0.52 in. of water. To select a fan, use the following equation:

Triple Stack System for Example 5

Figure 6. Triple Stack System for Example 5


Pressure Changes During Flow in Ducts

Figure 7. Pressure Changes During Flow in Ducts


Path (xx′)

Temp., °F

ρ, lbm/ft3

Δz (zxzx), ft

Δρ (ρa – ρxx), lbm/ft3

Δpse, in. of water [Eq. (14)]

1–2

1500

0.0202

(90 – 50)

+0.0548

+0.42

3–4

1000

0.0271

0

+0.0479

0

4–5

1000

0.0271

(25 – 95)

+0.0479

−0.64

6–7

250

0.0558

0

+0.0192

0

8–9

250

0.0558

(200 – 0)

+0.0192

+0.74

Net Thermal Gravity Effect

0.52


2.1 PRESSURE CHANGES IN SYSTEM

Figure 7 shows total and static pressure changes in a fan/duct system consisting of a fan with both supply and return air ductwork. Also shown are total and static pressure gradients referenced to atmospheric pressure.

For all constant-area sections, total and static pressure losses are equal. At diverging transitions, velocity pressure decreases, absolute total pressure decreases, and absolute static pressure can increase. The static pressure increase at these sections is known as static regain.

At converging transitions, velocity pressure increases in the direction of airflow, and absolute total and absolute static pressures decrease.

At the exit, total pressure loss depends on the shape of the fitting and the flow characteristics. Exit loss coefficients Co can be greater than, less than, or equal to one. Total and static pressure grade lines for the various coefficients are shown in Figure 7. Note that, for a loss coefficient less than one, static pressure upstream of the exit is less than atmospheric pressure (negative). Static pressure just upstream of the discharge fitting can be calculated by subtracting the upstream velocity pressure from the upstream total pressure.

At section 1, total pressure loss depends on the shape of the entry. Total pressure immediately downstream of the entrance equals the difference between the upstream pressure, which is zero (atmospheric pressure), and loss through the fitting. Static pressure of ambient air is zero; several diameters downstream, static pressure is negative, equal to the sum of the total pressure (negative) and the velocity pressure (always positive).

System resistance to airflow is noted by the total pressure grade line in Figure 7. Sections 3 and 4 include fan system effect pressure losses. To obtain the fan static pressure requirement for fan selection where fan total pressure is known, use

(17)

where

Ps = fan static pressure, in. of water
Pt = fan total pressure, in. of water
pv,o = fan outlet velocity pressure, in. of water

3. FLUID RESISTANCE

Duct system losses are the irreversible transformation of mechanical energy into heat. The two types of losses are (1) friction and (2) dynamic.

3.1 FRICTION LOSSES

Friction losses are caused by fluid viscosity and result from momentum exchange between molecules (in laminar flow) or between individual particles of adjacent fluid layers moving at different velocities (in turbulent flow). Friction losses occur along the entire duct length.

 Darcy and Colebrook Equations

For fluid flow in conduits, friction loss can be calculated by the Darcy equation:

(18)

where

Δpf = friction losses in terms of total pressure, in. of water
f = friction factor, dimensionless
L = duct length, ft
Dh = hydraulic diameter [Equation (24)], in.
V = velocity, fpm
ρ = density, lbm/ft3

In the region of laminar flow (Reynolds numbers less than 2300), the friction factor is a function of Reynolds number only. For completely turbulent flow (fully rough), the friction factor depends on duct surface roughness and internal protuberances (e.g., joints). Between the bounding limits of hydraulically smooth behavior (laminar flow) and fully rough behavior is a transitional zone where the friction factor depends on both roughness and Reynolds number. In both the transitional and fully rough (see Moody diagram: Figure 13 in Chapter 3) regions, the friction factor f is calculated by Colebrook’s equation (Colebrook 1938–1939). Because Colebrook’s equation cannot be solved explicitly for f, use iterative techniques (Behls 1971).

(19)

where

ε = material absolute roughness factor, ft
Re = Reynolds number

Reynolds number (Re) may be calculated by using the following equation.

(20)

where ν = kinematic viscosity, ft2/s.

For standard air and temperature between 40 and 100°F, Re can be calculated by

(21)

 Roughness Factors

Roughness factors listed in Table 1, column 3, are recommended for use with Equation (19). For increased calculation accuracy, use an absolute roughness factor from column 2.

Pressure Loss Correction Factor for Flexible Duct Not Fully Extended

Figure 8. Pressure Loss Correction Factor for Flexible Duct Not Fully Extended


Flexible Duct. For fully stretched and compressed flexible duct, use Equation (22) or Figure 8 (Abushakra et al. 2004; Culp 2011), where the multiplier PDCF is based on flexible duct with an absolute roughness ε = 0.003 ft. The resistance of flexible duct can be calculated using Fitting CD11-2 in the ASHRAE Duct Fitting Database (ASHRAE 2016). Flexible duct should be installed fully extended; its resistance when fully extended is increased approximately 50%. See Example 6 for the increase in resistance of flexible duct fully stretched and compressed relative to rigid spiral duct.

For commercial systems, flexible ducts should be

  • Limited to connections of rigid ducts to diffusers. For diffuser installation suggestions, see Figure 9. The purpose of limiting the offset to D/8 in Figure 9B is to minimize noise generation. Flexible duct should not be installed upstream of variable-air-volume (VAV) boxes.

    Commentary: The loss coefficient or pressure loss for flexible duct elbows, such as those in Figure 9A, can be obtained from the ASHRAE Duct Fitting Database (ASHRAE 2016), Fitting CD3-22 (r/D = 1.0) or CD3-23 (r/D = 1.5). Loss coefficients are for fully stretched elbows.

  • Limited to 6 ft maximum, fully stretched.

  • Installed without any radial compression.

Example 6.

Compare the total pressure resistance of 10 in., 6 ft installed length, galvanized steel spiral and flexible duct, 0% compressed (fully stretched), 4%, 15%, and 30% compressed. Airflow is 1000 cfm, air density is 0.075 lb/ft3, and absolute roughnesses ε of spiral round and flexible ducts are 0.004 ft and 0.003 ft. Calculate using the ASHRAE Duct Fitting Database [DFDB; ASHRAE (2016)].

Solution: See Table 2 for results.

(22)

with

(23)

where

PDCF = pressure drop correction factor
Kc = flexible duct compressed, percent
D = flexible duct diameter, in.
L = installed duct length, ft
LFE = duct length fully extended, ft


Table 1 Duct Roughness Factors

1

2

3

Duct Type/Material

Absolute Roughness ε, ft

Range

Roughness Category

Drawn tubing (Madison and Elliot 1946)

0.0000015

Smooth 0.0000015

PVC plastic pipe (Swim 1982)

0.00003 to 0.00015

Medium smooth 0.00015

Commercial steel or wrought iron (Moody 1944)

0.00015

 

Aluminum, round, longitudinal seams, crimped slip joints, 3 ft spacing (Hutchinson 1953)

0.00012 to 0.0002

 

Friction chart:

Galvanized steel, round, longitudinal seams, variable joints (Vanstone, drawband, welded. Primarily beaded coupling), 4 ft joint spacing (Griggs et al. 1987)

0.00016 to 0.00032

Average 0.0003

Galvanized steel, spiral seams, 10 ft joint spacing (Jones 1979)

0.0002 to 0.0004

 

Galvanized steel, spiral seam with 1, 2, and 3 ribs, beaded couplings, 12 ft joint spacing (Griggs et al. 1987)

0.00029 to 0.00038

 

Galvanized steel, rectangular, various type joints (Vanstone, drawband, welded. Beaded coupling), 4 ft spacinga (Griggs and Khodabakhsh-Sharifabad 1992)

0.00027 to 0.0005

 

Wright Friction Chart:

Galvanized steel, round, longitudinal seams, 2.5 ft joint spacing, ε = 0.0005 ft

Retained for historical purposes [See Wright (1945) for development of friction chart]

Flexible duct, nonmetallic and wire, fully extended (Abushakra et al. 2004; Culp 2011)

0.0003 to0.003

Medium rough 0.003

Galvanized steel, spiral, corrugated,b Beaded slip couplings, 10 ft spacing (Kulkarni et al. 2009)

0.0018 to 0.0030

 

Fibrous glass duct, rigid (tentative)c

 

Fibrous glass duct liner, air side with facing material (Swim 1978)

0.005

 

Fibrous glass duct liner, air side spray coated (Swim 1978)

0.015

Rough 0.01

Flexible duct, metallic corrugated, fully extended

0.004 to 0.007

 

Concrete (Moody 1944)

0.001 to 0.01

 

a Griggs and Khodabakhsh-Sharifabad (1992) showed that ε values for rectangular duct construction combine effects of surface condition, joint spacing, joint type, and duct construction (cross breaks, etc.), and that the ε-value range listed is representative.

b Spiral seam spacing was 4.65 in. with two corrugations between seams. Corrugations were 0.75 in. wide by 0.23 in. high (semicircle).

c Subject duct classified “tentatively medium rough” because no data available.



Table 2 Solution for Example 6

Duct

DFDB Fitting

ε, ft

Airflow, cfm

Diameter, in.

Velocity, fpm

Compression, %

PDCF *

Δpt, in. of water

% Δpt Increased

Flexible

CD11-2

0.003

1000

10

1833

(fully stretched)

1.0

0.043

48

Flexible

CD11-2

0.003

1000

10

1833

4

1.7

0.071

145

Flexible

CD11-2

0.003

1000

10

1833

15

3.5

0.148

410

Flexible

CD11-2

0.003

1000

10

1833

30

5.9

0.254

776

Galvanized steel, spiral

CD11-1

0.0004

1000

10

1833

NA

NA

0.029

Base


Diffuser Installation Suggestions

Figure 9. Diffuser Installation Suggestions


 Friction Chart

The friction chart (Figure 10) is a plot of the Darcy and Colebrook equations [Equations (18) and (19), respectively), where the absolute roughness is 0.0003 ft and the air is standard air (density = 0.075 lb/ft3)]. Figure 10 can be used for (1) duct construction/materials categorized as “average” in Table 1, (2) temperature variations of ±30°F from 70°F, (3) elevations to 1500 ft, and (4) duct pressures from –20 to +20 in. of water relative to ambient pressure. These individual variations in temperature, elevation, and duct pressure result in duct losses within ±5% of the standard air friction chart.

The friction chart was changed in 1985 from an absolute roughness of 0.0005 ft to 0.0003 ft based on research by Griggs et al. (1987), who found that the roughness factor is affected by the material surface, joint spacing, and type of joint. The Wright friction chart appeared in the Handbook from 1946 to 1981. This chart was based on an absolute roughness ε = 0.0005 ft, primarily because of the 2.5 ft joint spacing. In 1985 the friction chart was changed to ε = 0.0003 ft because joint spacing was increasing. For the relative effect of straight duct resistance between charts, see Figure 11. For a 10 in. diameter duct at 2000 fpm (1091 cfm), the resistance decreased 5 to 6%.

 Noncircular Ducts

A momentum analysis can relate average wall shear stress to pressure drop per unit length for fully developed turbulent flow in a passage of arbitrary shape but uniform longitudinal cross-sectional area. This analysis leads to the definition of hydraulic diameter:

(24)

where

Dh = hydraulic diameter, in.
A = duct area, in2
P = perimeter of cross section, in.

Although hydraulic diameter is often used to correlate noncircular data, exact solutions for laminar flow in noncircular passages show that this causes some inconsistencies. No exact solutions exist for turbulent flow. Tests over a limited range of turbulent flow indicated that fluid resistance is the same for equal lengths of duct for equal mean velocities of flow if the ducts have the same ratio of cross-sectional area to perimeter. From experiments using round, square, and rectangular ducts having essentially the same hydraulic diameter, Huebscher (1948) found that each, for most purposes, had the same flow resistance at equal mean velocities. Tests by Griggs and Khodabakhsh-Sharifabad (1992) also indicated that experimental rectangular duct data for airflow over the range typical of HVAC systems can be correlated satisfactorily using Equation (19) together with hydraulic diameter, particularly when a realistic experimental uncertainty is accepted. These tests support using hydraulic diameter to correlate noncircular duct data.

Rectangular Ducts. Huebscher (1948) developed the relationship between rectangular and round ducts that is used to determine size equivalency based on equal flow, resistance, and length. This relationship, Equation (25), is the basis for Table 3.

(25)

where

De = circular equivalent of rectangular duct for equal length, fluid resistance, and airflow, in.
a = length one side of duct, in.
b = length adjacent side of duct, in.

To determine equivalent round duct diameter, use Table 3. Equations (18) and (19) must be used to determine pressure loss.

Flat Oval Ducts. To convert round ducts to flat oval sizes, use Table 4, which is based on Equation (26) (Heyt and Diaz 1975), the circular equivalent of a flat oval duct for equal airflow, resistance, and length. Equations (18) and (19) must be used to determine friction loss.

(26)

where AR is the cross-sectional area of flat oval duct defined as

(27)

and the perimeter P is calculated by

(28)

where

P = perimeter of flat oval duct, in.
A = major axis of flat oval duct, in.
a = minor axis of flat oval duct, in.

3.2 DYNAMIC LOSSES

Dynamic losses result from flow disturbances caused by duct-mounted equipment and fittings that change flow direction (elbows), area changes (transitions), and converging/diverging junctions. For a detailed discussion of hydraulic networks, consult Idelchik et al. (1994).

 Local Loss Coefficients

The dimensionless coefficient C is used for fluid resistance because this coefficient has the same value in dynamically similar streams (i.e., streams with geometrically similar stretches, equal Reynolds numbers, and equal values of other criteria necessary for dynamic similarity). The fluid resistance coefficient represents the ratio of total pressure loss to velocity pressure at the referenced cross section:

(29)

where

C = local loss coefficient, dimensionless
Δpt = total pressure loss, in. of water
ρ = density, lbm/ft3
V = velocity, fpm
pv = velocity pressure, in. of water

For all fittings, except junctions, total pressure loss is calculated by Equation (30):

(30)

where

Δpt = total pressure loss of fitting, in. of water
Co = local loss coefficient of fitting, dimensionless
pv,o = velocity pressure at section o of fitting, in. of water

Dynamic loss is based on the actual velocity in the duct, not the velocity in an equivalent circular duct. For the cross section to reference a fitting loss coefficient, see step 5 in the section on HVAC Duct Design Procedures. Where necessary (e.g., unequal-area fittings), convert a loss coefficient from section o to section 1 using Equation (31), where V is the velocity at the respective sections.

(31)

Friction Chart for Round Duct (ρ = 0.075 lbm/ft3 and ε = 0.0003 ft)

Figure 10. Friction Chart for Round Duct (ρ = 0.075 lbm/ft3 and ε = 0.0003 ft)


Table 3 Equivalent Rectangular Duct Dimensions for Equal Friction and Airflow*

Circular Duct Diameter, in.

Length of One Side of Rectangular Duct a, in.

4

5

6

7

8

9

10

12

14

16

18

20

22

24

26

28

30

32

34

36

Length Adjacent Side of Rectangular Duct b, in.

5

5

                                     

5.5

6

5

                                   

6

8

6

                                   

6.5

9

7

6

                                 

7

11

8

7

                                 

7.5

13

10

8

7

                               

8

15

11

9

8

                               

8.5

17

13

10

9

                               

9

20

15

12

10

8

                             

9.5

22

17

13

11

9

                             

10

25

19

15

12

10

9

                           

10.5

29

21

16

14

12

10

                           

11

32

23

18

15

13

11

10

                         

11.5

 

26

20

17

14

12

11

                         

12

 

29

22

18

15

13

12

                         

12.5

 

32

24

20

17

15

13

                         

13

 

35

27

22

18

16

14

12

                       

13.5

 

38

29

24

20

17

15

13

                       

14

   

32

26

22

19

17

14

                       

14.5

   

35

28

24

20

18

15

                       

15

   

38

30

25

22

19

16

14

                     

16

   

45

36

30

25

22

18

15

                     

17

     

41

34

29

25

20

17

16

                   

18

     

47

39

33

29

23

19

17

                   

19

     

54

44

38

33

26

22

19

18

                 

20

       

50

43

37

29

24

21

19

                 

21

       

57

48

41

33

27

23

20

                 

22

       

64

54

46

36

30

26

23

20

               

23

         

60

51

40

33

28

25

22

               

24

         

66

57

44

36

31

27

24

22

             

25

           

63

49

40

34

29

26

24

             

26

           

69

54

44

37

32

28

26

24

           

27

           

76

59

48

40

35

31

28

25

           

28

             

64

52

43

38

33

30

27

26

         

29

             

70

56

47

41

36

32

29

27

         

30

             

76

61

51

44

39

35

31

29

28

       

31

             

82

66

55

47

41

37

34

31

29

       

32

               

89

71

59

51

44

40

36

33

31

       

33

               

96

76

64

54

48

42

38

35

33

30

     

34

                 

82

68

58

51

45

41

37

35

32

     

35

                 

88

73

62

54

48

44

40

37

34

32

   

36

                 

95

78

67

58

51

46

42

39

36

34

   

37

                 

101

83

71

62

55

49

45

41

38

36

34

 

38

                 

108

89

76

66

58

52

47

44

40

38

36

 

39

                   

95

80

70

62

55

50

46

43

40

37

36

40

                   

101

85

74

65

58

53

49

45

42

39

37

41

                   

107

91

78

69

62

56

51

47

44

41

39

42

                   

114

96

83

73

65

59

54

50

46

44

41

43

                   

120

102

88

77

69

62

57

53

49

46

43

44

                     

107

93

81

73

66

60

55

51

48

45

45

                     

113

98

86

76

69

63

58

54

50

47

46

                     

120

103

90

80

72

66

61

56

53

49

47

                     

126

108

95

84

76

69

64

59

55

52

48

                     

133

114

100

89

80

73

67

62

58

54

49

                     

140

120

105

93

84

76

70

65

60

56

50

                     

147

126

110

98

88

80

73

68

63

59

51

                       

132

115

102

92

83

76

71

66

61

52

                       

139

121

107

96

87

80

74

69

64

53

                       

145

127

112

100

91

83

77

71

67

54

                       

152

133

117

105

95

87

80

74

70

55

                         

139

123

110

99

91

84

78

72

56

                         

145

128

114

104

95

87

81

75

57

                         

151

134

119

108

98

91

84

78

58

                         

158

139

124

112

102

94

87

81

59

                         

165

145

130

117

107

98

91

85

60

                         

172

151

135

122

111

102

94

88

* Table based on Equation (25).



Table 4 Equivalent Flat Oval Dimensions*

Circular Duct Diameter, in.

Minor Axis a, in.

3

4

5

6

7

8

9

10

11

12

14

16

18

20

22

24

30

Major Axis A, in.

5

8

                               

5.5

9

7

                             

6

11,12

                               

6.5

14

9,10

8

                           

7

17

12

 

8

                         

7.5

19

13

10

9

                         

8

22

15

11

                           

8.5

 

17,18

13,14

11

10

                       

9

 

20,21

 

12

 

10

                     

9.5

   

16

14

12

11

                     

10

   

18,19

15

13

                       

10.5

   

21

17

15

13

                     

11

     

19

16

14

12

12

                 

11.5

     

20

18

 

14

13

                 

12

     

22,23

 

16,17

15

14

                 

12.5

     

25,26

20,21

     

14

               

13

     

28

 

19

17

16

 

14

             

13.5

     

30,31

 

21

18

                   

14

     

33

 

22

20

18

16,17

15

             

14.5

     

34,36

 

24,25

22

19

                 

15

     

37

 

27

23

21

19

17,18

             

15.5

     

41

       

20

               

16

     

44,47

 

30,32

 

23,24

22

20

             

17

         

33,35,36

 

26,27

24,25

21,23

20

           

18

         

38,39

 

29,30

 

25,26

22

           

19

         

43,46

 

32,34,35

 

28,29

23

22

         

20

         

49,52

 

37,38,40

 

31,32

25,27

24

         

21

         

55,58

 

41

 

34

28,30

25

23,24

       

22

         

61

 

45,48

 

36,37,39

31,33

27,29

26

       

23

             

51,54

 

40,43

34,36

30

27

26

     

24

             

57,60

 

47

39

32,33

29

28

     

25

             

63

 

50

42

35

31,32

29

     

26

             

67,70,73

 

53,56

45

38

34,35

31

     

27

             

76,79

 

59,62

49

41

37

33

     

28

                 

65

52,55

44

40

36

     

29

                 

69,72

58

47

43

39

35

   

30

                 

75,78

61,64

51,54

46

42

38

   

31

                 

81

67

57

49

45

41

37

 

32

                   

71,74

60

53

48

 

40

 

33

                   

77,80

66

56

51

44

   

34

                     

69

59,62

 

47

43

 

35

                     

73,76

65

55,58

50

46

 

36

                     

79

68

61

53

49

 

37

                       

71

64

57

52

43

38

                       

75,78

67

60

55

 

39

                       

81

70,73

63

59

46

40

                         

77

66,69

62

49

41

                         

80

72

65

52

42

                           

75

68

55

43

                           

79

71

 

44

                           

82

74

58

45

                             

77

61

46

                             

81

65

47

                               

68

48

                               

71

49

                               

74

50

                               

77

51

                               

80

52

                               

81

* Table based on Equation (26).


Plot Illustrating Relative Resistance of Roughness Categories

Figure 11. Plot Illustrating Relative Resistance of Roughness Categories


For converging and diverging flow junctions, total pressure loss through the straight (main) section is calculated by

(32)

where

Δpt,s = total pressure loss across straight-through section s of junction, in. of water
Cs = local loss coefficient referenced to s section of junction, dimensionless
pv,s = velocity pressure at section s, in. of water

For total pressure loss through the branch section,

(33)

where

Δpt,b = total pressure loss across branch b section of junction, in. of water
Cb = local loss coefficient referenced to b section of junction, dimensionless
pv,b = velocity pressure at section b, in. of water

The junction of two parallel streams moving at different velocities is characterized by turbulent mixing of the streams, accompanied by pressure losses. In the course of this mixing, particles moving at different velocities exchange momentum, resulting in equalization of the velocity distributions in the common stream. The jet with higher velocity loses part of its kinetic energy by transmitting it to the slower jet. The loss in total pressure before and after mixing is always large and positive for the higher-velocity jet, and increases with an increase in the amount of energy transmitted to the lower-velocity jet. Consequently, the local loss coefficient [Equation (29)] is always positive. Energy stored in the lower-velocity jet can increase because of mixing. The loss in total pressure and the local loss coefficient can, therefore, also have negative values for the lower-velocity jet (Idelchik et al. 1994).

 Duct Fitting Database

Loss coefficients for more than 220 round, flat oval, and rectangular fittings are available in the ASHRAE Duct Fitting Database [DFDB; ASHRAE (2016)]. Also included are the pressure loss for round duct (CD11-1), flexible duct (CD11-2), rectangular duct (CR11-1), and flat oval (CF11-1) duct, as well as the following design tools:

  • CD11-3, Straight Duct, Round, Velocity Limited

  • CD11-4, Straight Duct, Round, Friction Rate Constant

  • CD11-5, Straight Duct, Round, Minimum Velocity

Table 5 Duct Fitting Codes

Fitting Function

Geometry

Category

Sequential Number

S: Supply

D: round (Diameter)

1. Entries

1, 2, 3... n

   

2. Exits

 

E: Exhaust/Return

R: Rectangular

3. Elbows

 
   

4. Transitions

 

C: Common (supply and return)

F: Flat oval

5. Junctions

 
 

6. Obstructions

 
 

7. Fan and system interactions

 
   

8. Duct-mounted equipment

 
   

9. Dampers

 
   

10. Hoods

 
   

11. Straight duct

 



Table 6 8 in. VAV Box Data

Airflow, cfm

Δps, in. of water

Inlet Velocity, fpm

Outlet Velocity, fpm

pv, in, in. of water

pv, out, in. of water

Δpv, in. of water

Δpt, in. of water

1

2

3

4

5

6

7

8

350

0.053

1003

420

0.063

0.011

0.052

0.105

500

0.109

1432

600

0.128

0.022

0.105

0.214

700

0.213

2005

840

0.251

0.044

0.207

0.420

900

0.353

2578

1080

0.414

0.073

0.342

0.695

Δps = static pressure difference

Δpt = total pressure difference at standard air conditions

pv, in = inlet velocity pressure at standard air conditions

pv, out = outlet velocity pressure at standard air conditions

Δpv = velocity pressure difference at standard air conditions


Commentary: CD11-3 determines the size of a duct knowing airflow such that the design velocity is not exceeded. CD11-4 is for sizing duct systems by the equal friction method, knowing the design (target) friction rate and airflow. CD4-11 determines the duct size for industrial systems that must maintain a minimum velocity to convey particulates.

Example 8 uses CD11-3 in the equal friction and static regain designs, and CD11-4 for the equal friction design.

The fittings are numbered (coded) as shown in Table 5. Entries and converging junctions are only in the exhaust/return portion of systems. Exits and diverging junctions are only in supply systems. Equal-area elbows, obstructions, and duct-mounted equipment are common to both supply and exhaust systems. Transitions and unequal-area elbows can be either supply or exhaust fittings. Fitting ED5-1 is an Exhaust fitting with a round shape (Diameter). The number 5 indicates that the fitting is a junction, and 1 is its sequential number. Fittings SR31 and ER3-1 are Supply and Exhaust fittings, respectively. The R indicates that the fitting is Rectangular, and the 3 identifies the fitting as an elbow. Note that the cross-sectional areas at sections 0 and 1 are not equal. Otherwise, the elbow would be a Common fitting such as CR3-6.

Terminal Unit Loss Coefficients. Manufacturers’ data for terminal units are not useful for duct design because they are given in terms of static pressure resistance and velocity pressure at standard air conditions (0.075 lbm/ft3). The total pressure loss coefficient for the 8 in. terminal used in Example 7 is calculated from manufacturer’s published data (Table 6: Columns 1, 2, and 7) and plotting Δpv,in versus Δpt (Figure 12). The loss coefficient is 1.68 and is applicable for any elevation (air density). The total pressure loss (Δpt) in Table 6 is only useful for projects at sea level. ASHRAE Standard 130-2016, Section 5.2, covers the laboratory test for total pressure loss and the calculation of the loss coefficient. In the ASHRAE Duct Fitting Database (ASHRAE 2016), the single-duct reheat VAV box is the CD8-series.

VAV Box Loss Coefficient Plot

Figure 12. VAV Box Loss Coefficient Plot


3.3 DUCTWORK SECTIONAL LOSSES

 Darcy-Weisbach Equation

Total pressure loss in a duct section is calculated by combining Equations (18) and (29) in terms of Δp, where ΣC is the summation of local loss coefficients in the duct section. Each fitting loss coefficient must be referenced to that section’s velocity pressure.

(34)

4. FAN/SYSTEM INTERFACE

 Fan Inlet and Outlet Conditions

Fan performance data measured in the field may show lower performance capacity than manufacturers’ ratings. The most common causes of deficient performance of the fan/system combination are poor outlet connections, nonuniform inlet flow, and swirl at the fan inlet. These conditions alter the fan’s aerodynamic characteristics so that its full flow potential is not realized. One bad connection can reduce fan performance below its rating.

Normally, a fan is tested with open inlets and a section of straight duct attached to the outlet (AMCA Standard 210). This setup results in uniform flow into the fan and efficient static pressure recovery on the fan outlet. If good inlet and outlet conditions are not provided in the design of duct systems, fan performance suffers.

Figure 13 shows deficient fan performance resulting from poor inlet and outlet connections to ductwork. Point 1 is the fan/system operating point without taking into account poor inlet and/or outlet conditions. Point 2 is the system operating point when the apparent resistance of poor connections is included in the calculations. Point 4 is the operating point on the original fan performance curve, taking into consideration the apparent system resistance of poor fan/system connections. Point 3 is the fan operating point on the original system curve when the apparent resistance of poor inlet and/or fan connections is not taken into account. The airflow difference between points 2 and 4 represents the deficiency in airflow from design airflow.

 Fan System Effect Coefficients

The system effect concept was formulated by Farquhar (1973) and Meyer (1973); the magnitudes of the system effect, called system effect factors, were determined experimentally by the Air Movement and Control Association International (AMCA 2011a; Brown 1973; Clarke et al. 1978). The system effect factors, converted to local loss coefficients, are in the ASHRAE Duct Fitting Database (ASHRAE 2016) for both centrifugal and axial fans. Fan system effect coefficients are only an approximation. Fans of different types and even fans of the same type, but supplied by different manufacturers, do not necessarily react to a system in the same way. Therefore, judgment based on experience must be applied to any design.

Deficient System Performance with System Effect Ignored

Figure 13. Deficient System Performance with System Effect Ignored


Fan Outlet Conditions. Fans intended primarily for duct systems are usually tested with an outlet duct in place (AMCA Standard 210). Figure 14 shows the changes in velocity profiles at various distances from the fan outlet. For 100% recovery, the duct, including transition, must meet the requirements for 100% effective duct length [Le (Figure 14)], which is calculated as follows:

For Vo > 2500 fpm,

(35)

For Vo2500 fpm,

(36)

where

Vo = duct velocity, fpm
Le = effective duct length, ft
Ao = duct area, in2

Centrifugal fans should not abruptly discharge to the atmosphere. A diffuser design should be selected from Fitting SR7-2 or SR7-3. Consult the SR7-series fittings of the ASHRAE Duct Fitting Database (ASHRAE 2016) for guidance in the design of fan/ductwork connections.

Fan Inlet Conditions. For rated performance, air must enter the fan uniformly over the inlet area in an axial direction without prerotation. Nonuniform flow into the inlet is the most common cause of reduced fan performance. Such inlet conditions are not equivalent to a simple increase in system resistance; therefore, they cannot be treated as a percentage decrease in the flow and pressure from the fan. A poor inlet condition results in an entirely new fan performance.

Establishment of Uniform Velocity Profile in Straight Fan Outlet Duct (Adapted by permission from AMCA Publication 201)

Figure 14. Establishment of Uniform Velocity Profile in Straight Fan Outlet Duct (Adapted by permission from AMCA Publication 201)


Inlet Duct Connections Causing Inlet Spin (Adapted by permission from AMCA Publication 201)

Figure 15. Inlet Duct Connections Causing Inlet Spin (Adapted by permission from AMCA Publication 201)


Fitting ED7-2 (Fan Inlet, Centrifugal Fan, SISW, with 4-Gore Elbow) [ASHRAE Duct Fitting Database (ASHRAE 2016)]

Figure 16. Fitting ED7-2 (Fan Inlet, Centrifugal Fan, SISW, with 4-Gore Elbow) [ASHRAE Duct Fitting Database (ASHRAE 2016)]


Inlet spin may arise from many different approach conditions, and sometimes the cause is not obvious. Figure 15 shows some common duct connections that cause inlet spin. Inlet spin can be avoided by providing an adequate length of duct between the elbow and the fan inlet, as shown by Figure 16. Two L/Do duct lengths upstream of the fan inlet reduces swirl and pressure loss (loss coefficient) by approximately 45% (Table 7).

Table 7 ED7-2 Loss Coefficients (see Figure 16)

L/Do

L/Do

0

2

5

10

0.5

1.80

1.00

0.53

0.53

0.75

1.40

0.80

0.40

0.40

1.0

1.20

0.67

0.33

0.33

1.5

1.10

0.60

0.33

0.33

2.0

1.00

0.53

0.33

0.33

4.0

0.67

0.40

0.22

0.22


Fans within plenums and cabinets or next to walls should be located so that air may flow unobstructed into the inlets. Fan performance is reduced if the space between the fan inlet and the enclosure is too restrictive. System effect coefficients for fans in an enclosure or adjacent to walls are listed under Fitting ED7-1. How the airstream enters an enclosure in relation to the fan inlets also affects fan performance. Plenum or enclosure inlets or walls that are not symmetrical with the fan inlets cause uneven flow and/or inlet spin.

5. MECHANICAL EQUIPMENT ROOMS

In the initial phase of building design, the design engineer seldom has sufficient information to render the optimum HVAC design for the project, and its space requirements are often based on percentage of total area or other rule of thumb. The final design is usually a compromise between what the engineer recommends and what the architect can accommodate. Total mechanical and electrical space requirements range between 4 and 9% of gross building area, with most buildings in the 6 to 9% range. This range includes space for HVAC, electrical, plumbing, and fire protection equipment, as well as vertical shaft space for mechanical and electrical distribution through the building.

 Outdoor Air Intake and Exhaust Air Discharge Locations

A key factor in the location of mechanical equipment rooms is the source of outdoor air. If the air intake or exhaust system is not well designed, contaminants from nearby outdoor sources (e.g., vehicle exhaust) or from the building itself (e.g., laboratory fume hood exhaust) can enter the building with insufficient dilution. Poorly diluted contaminants may cause odors, health impacts, and reduced indoor air quality. Examples are toxic stack exhausts, automobile and truck traffic, kitchen cooking hoods, evaporative cooling towers, building general exhaust air, trash dumpsters, stagnant water bodies, snow and leaves, rain and fog, plumbing vents, vandalism, and terrorism.

Chapter 45 of the 2019 ASHRAE Handbook—HVAC Applications discusses proper design of exhaust stacks and placement of air intakes to avoid adverse air quality impacts. Experience provides some general guidelines on air intake placement. Unless dispersion modeling analysis is conducted, air intakes should never be located on the roof in the same architectural screen enclosure as exhaust outlets. If exhaust is discharged from several locations on the roof, intakes should be located to minimize contamination. Typically, this means maximizing separation distance. Where all exhausts of concern are emitted from a single, relatively tall stack or tight cluster of stacks, a possible intake location might be close to the base of this tall stack, if this location is not adversely affected by other exhaust locations, or is not influenced by tall adjacent structures creating downwash. Architectural screens placed around rooftop equipment to reduce noise or hide equipment interact with the windflow patterns on the roof and can adversely affect exhaust dilution. Chapter 45 of the 2019 ASHRAE Handbook—HVAC Applications describes a method to account for these screens by modifying the physical stack height.

When wind is perpendicular to the upwind wall, air flows up and down the wall, dividing at about two-thirds up the wall. The downward flow creates ground-level swirl that stirs up dust and debris. To take advantage of the natural separation of wind over the upper and lower halves of a building, toxic or nuisance exhausts should be located on the roof and intakes on the lower one-third of the building, but high enough to avoid wind-blown dust, debris, and vehicle exhaust. If ground-level sources are major sources of contaminants, rooftop intake is desirable.

Buildings over three stories usually require vertical shafts to consolidate mechanical, electrical, and telecommunication distribution through the facility. Vertical shafts should be located in or adjacent to mechanical/fan rooms and as far as possible from noise-sensitive areas. In general, duct shafts with an aspect ratio of 2:1 to 4:1 are easier to develop than large square shafts. The rectangular shaft also facilitates transition from equipment in the fan rooms to the shaft.

Fan rooms in a basement or at street level should be avoided. These locations are a security concern because harmful substances could easily be introduced. Using louvers at these locations is also a concern because debris, leaves, and snow may fill the area, resulting in safety, health, and fan performance concerns. Loading docks and nearby parking areas may also compromise ventilation air quality.

 Equipment Room Locations

Mechanical equipment rooms, including air-handling units, should be centrally located to centralize maintenance and operation. But, for many reasons, not all equipment rooms can be centrally located in the building. In any case, equipment should be kept together whenever possible to minimize space requirement, centralize maintenance and operation, and simplify electrical systems. All HVAC air system equipment rooms should have space for maintaining equipment and the replacement of fans, coils and other key equipment.

High-rise buildings may opt for decentralized fan rooms for each floor, or for more centralized service with one mechanical/fan room serving the lower 10 to 20 floors, one serving the middle floors of the building, and one at the roof serving the top floors.

Decentralized Equipment Rooms. Locate decentralized mechanical equipment rooms as far as possible from noise-sensitive areas, and surround equipment rooms with buffer zones such as toilet and storage rooms, as well as elevator, stair, and duct shafts. Figure 17 shows various core locations from poor to best. The number of decentralized fan rooms required depends largely on total floor area and any fan system power limitation imposed by codes or standards (e.g., ASHRAE Standard 90.1-2016, section 6.5.3.1). When decentralized air systems are located centrally to the spaces served, duct systems are shorter, occupy less volume, use less power, are quieter, and are less expensive. Pointing out these advantages can often help to convince architects to make desirable decentralized locations available.

6. DUCT DESIGN

6.1 DESIGN CONSIDERATIONS

 HVAC System Air Leakage

See Chapter 19 of the 2020 ASHRAE Handbook—HVAC Systems and Equipment for (1) sealant specifications, and (2) the rationale for HVAC system sealing and leakage testing.

System Sealing. All ductwork and plenum transverse joints, longitudinal seams, and duct penetrations should be sealed. Openings for rotating shafts should be sealed with bushings or other devices that minimize air leakage but that do not interfere with shaft rotation or prevent thermal expansion. Spiral lock seams need not be sealed. Duct-mounted equipment, such as terminal units, reheat coils, access doors, sound attenuators, balancing dampers, control dampers, and fire dampers, should be specified as low leakage so that the system can meet the air leakage acceptance criteria set by the designer, standards, and codes. Recommended specifications for duct-mounted equipment are provided later in this section.

Comparison of Various Mechanical Equipment Room Locations (Schaffer 2005)

Figure 17. Comparison of Various Mechanical Equipment Room Locations (Schaffer 2005)


Sealing that would void product listings (e.g., for fire/smoke or volume control dampers) is not required. It is, however, recommended that the design engineer specify low-leakage duct-mounted components. For example, some UL-listed and -labeled fire/smoke dampers allow sealing and gasketing of breakaway duct/sleeve connections; all can provide sealed non-breakaway duct/sleeve connections.

Scope. It is recommended that supply air (both upstream and downstream of the VAV box primary air inlet damper when used) and independent exhaust air systems be tested for air leakage after construction at operating conditions using ASHRAE Proposed Standard 215 (under development, and expected to be published in 2018) to verify (1) good workmanship, and (2) the use of low-leakage components as required to achieve the design allowable system air leakage. To ensure that a system passes its air leakage test at operating conditions, sufficient ductwork sections should be leak tested during construction. Leakage of duct-mounted components should be determined by specification and certified leakage data provided with equipment submittals. Leakage of air-handling units should be determined by specification and verification leakage tests.

Independent exhaust air system: air discharged from a space to the outdoors by a system not coupled to supply or return air systems.

Acceptance Criteria. To enable proper accounting of leakage-related impacts on fan energy and space conditioning loads, the allowable system air leakage for each fan system should be established by the design engineer as a percentage of fan airflow at the maximum system operating conditions. The recommended maximum system leakage is 5% of design airflow. Exceptions: supply and return ductwork sections that leak directly to/from outdoors and exhaust system ductwork sections that draw in indoor air through leaks should be limited to 2%.

Equation (37) is for use in a leakage test during construction to ensure that ductwork will meet the leakage specification. This equation translates system fractional air leakage to test section leakage class, as specified by ASHRAE Standard 90.1-2016, section 6.4.4.2.2.

(37)

where

CL,section = test section leakage class, cfm per (in. of water)0.65 per 100 ft2 of duct surface area
Qfan = maximum fan airflow that would occur during operation, cfm
Qleak, frac = system leakage fraction corresponding to maximum fan airflow that would occur during operation, %
Asystem = total system duct surface area, ft2
Δpsection = test section static pressure difference corresponding to maximum fan airflow that would occur during operation, in. of water

Equation (37) shows that leakage class depends on fractional air leakage and normalized fan airflow (Qfan/Asystem), and varies inversely with the pressure difference raised to the 0.65 power. For example, to achieve 3% leakage for ductwork with Qfan/Asystem = 2 cfm per ft2 of duct surface area and Δpsection = 3 in. of water, the required leakage class is 2.9 cfm per (in. of water)0.65 per 100 ft2 of duct surface area. With Δpsection = 0.5 in. of water instead (six times less), the required leakage class is about three times greater (9.4).

The maximum acceptable air leakage for a test section corresponding to the leakage class determined by Equation (37) can be expressed by Equation (38).

(38)

where where

Qleak,section = test section air leakage, cfm
Asection = test section duct surface area, ft2

Equations (37) and (38) can be combined so that the maximum acceptable air leakage for a test section during construction is simply a function of system fractional leakage, normalized fan airflow (Qfan/Asystem), and section duct surface area:

(39)

Thus, for air leakage tests during construction, the maximum acceptable leakage for a ductwork section is given by Equation (38) or (39). Duct surface area should be calculated in accordance with European Standard EN 14239. The test pressure for each section should be specified by the design engineer based on the maximum static pressure for that section that would occur during operation at maximum fan airflow.

Example 7.

The system depicted by Figure 18 has the characteristics summarized by Table 8. For a maximum acceptable leakage of 3% of the 5000 cfm maximum fan airflow, which is 150 cfm total, what is the maximum allowable ductwork leakage in (1) each section that is to be tested at the pressures noted, and (2) sections 4 and 5 when leak tested together?

Solution: The calculations and maximum allowable leakage are also summarized in Table 8. Note that adjacent sections with the same static pressure can be grouped for leakage testing. In this case, Sections 4 and 5 can be grouped. The allowable leakage for Sections 4 and 5 when tested individually is 10 cfm and 48 cfm respectively. The allowable leakage for Sections 4 and 5 when tested together is 58 cfm.


Table 8 Solution for Example 7

Section

Section Inlet Flow, cfm

Asection, ft2

Section Static Pressure, in. of water

 

Section Leakage Class, cfm per 100 ft2 per in. of water0.65

 

Section Allowable Leakage, cfm

Input

Equation (37)

Equation (38) or (39)

1

5000

500

3.0

 

2.4

 

24

2

2000

667

1.0

 

4.8

 

32

3

3000

750

2.0

 

3.1

 

36

4

1000

200

1.0

 

4.8

 

10

5

2000

1000

1.0

 

4.8

 

48

Total

 

3117

       

150

4 and 5

3000

1200

1.0

 

4.8

 

58


Duct Layout for Example 7

Figure 18. Duct Layout for Example 7


Recommended Specification for Duct-Mounted Equipment. Duct-mounted component leakage is controlled by specification and certified leakage data provided with equipment submittals. The following are recommended leakage-related specifications for duct-mounted equipment.

  • Terminal Units. Seal longitudinal seams of casings, inlet face of casings, and inlet collars with mastic. Seal damper shaft penetrations of casings. Casing leakage for the basic terminal unit should not exceed 4.5 cfm at 1.0 in. of water static pressure differential. Terminal unit leakage with an access door should not exceed 4.6 cfm at 1.0 in of water. Testing should be by an accredited laboratory. Leakage tests should comply with ASHRAE Standard 130.

    Access doors in terminal unit casings should comply with AMCA Standard 500-D, and leakage rates should be certified per AMCA (2013) Publication 511. Access door (frame not included) leakage should not exceed 0.5 cfm at 10 in. of water static pressure differential.

  • Electric Reheat Coils. Flange-mount electric coils with a gasket. Coil leakage should not exceed 0.5 cfm at 1.0 in. of water static pressure differential. Tests should be by an accredited laboratory. Leakage tests should be in compliance with ASHRAE Standard 126.

  • Hot-Water Reheat Coils. Flange-mount hot-water coils with a gasket in an insulated plenum or casing. Seal all seams and casing penetrations for supply and return water tubes. Coil casing leakage (not counting transverse joints) should not exceed 0.5 cfm at 1.0 in. of water static pressure differential. An accredited laboratory should perform leakage tests in compliance with ASHRAE Standard 126.

  • Access Doors. Access door leakage (excluding the frame) should not exceed 0.5 cfm at 10 in. of water static pressure differential. Leakage tests should comply with AMCA Standard 500-D, and leakage rates certified per AMCA (2013) Publication 511.

  • Attenuators. Sound attenuator casing seams should be sealed at the factory if used in-line with the ductwork. Attenuators stacked in plenums do not have to be sealed, but plenums should be sealed.

  • Fire/Smoke Dampers. These dampers should be installed in accordance with the manufacturer’s UL installation instructions. Each fire damper should be furnished with a UL-approved sleeve. Sleeve seams should be continuously welded or sealed, and the transverse joint should be a sealed UL-approved flanged duct sleeve connection (break-away or non-break-away).

  • Balancing Dampers. Balancing damper casing seams should be continuously welded or sealed, and the shaft penetrating the casing should have seals.

  • Control Dampers. Control damper shafts penetrating ducts should have seals.

Recommended Specification for Air-Handling Units. Refer to Chapter 19 of the 2020 ASHRAE Handbook—HVAC Systems and Equipment for leakage-related specifications for air-handling units.

Responsibilities. The engineer should

  • Specify HVAC system components, duct-mounted equipment, sealants, and sealing procedures that together will meet the system airtightness design objective.

  • Inspect the system during construction for quality of workmanship and to verify that correct duct-mounted components and air-handling units are installed.

  • Specify the construction-stage ductwork leakage test standard or procedures.

  • Specify the construction-stage test pressures to the nearest 0.1 in. of water expected during operation at design conditions and the maximum allowable air leakage.

  • Review and approve the sheet metal and test contractors’ leakage test reports. If any system has a leakage failure, the engineer should discuss remedies with the sheet metal contractor, vendor, and/or owner’s representative.

The sheet metal contractor should

  • Construct the system using quality workmanship and correct duct-mounted components and air-handling units. If any installed duct-mounted equipment appears to be leakage suspect, the contractor should discuss remedies with the engineer and/or owner’s representative.

  • Conduct ductwork leakage pressurization tests during construction. As a minimum, 25% of the ductwork system (based on duct surface area) should be tested during construction, and another 25% if any of the initial sections fail. If any section of the second 25% fails, the entire ductwork system should be leak tested.

  • Provide connections for test apparatus, and separate test sections from each other as needed so that the test apparatus capacity is not exceeded.

  • Report test results and, where required, take corrective action to seal ductwork and absorb the cost for conducting related additional leak tests.

The test contractor should

  • Conduct the operating system leakage test in compliance with ASHRAE Proposed Standard 215 (expected to publish in 2018).

  • Report test results, including reasons for any failures.

It should be the responsibility of the owner or owner’s representative to provide direction upon request.

 Fire and Smoke Control

Because duct systems can convey smoke, hot gases, and fire from one area to another and can accelerate a fire within the system, fire protection is an essential part of air-conditioning and ventilation system design. Generally, fire safety codes require compliance with the standards of national organizations. NFPA Standard 90A examines fire safety requirements for (1) ducts, connectors, and appurtenances; (2) plenums and corridors; (3) air outlets, air inlets, and fresh air intakes; (4) air filters; (5) fans; (6) electric wiring and equipment; (7) air-cooling and -heating equipment; (8) building construction, including protection of penetrations; and (9) controls, including smoke control.

Fire safety codes often refer to the testing and labeling practices of nationally recognized laboratories, such as Factory Mutual and Underwriters Laboratories (UL). UL’s annual Building Materials Directory lists fire and smoke dampers that have been tested and meet the requirements of UL Standards 555 and 555S. This directory also summarizes maximum allowable sizes for individual dampers and assemblies of these dampers. Fire dampers are 1.5 h or 3 h fire-rated. Smoke dampers are classified by (1) temperature degradation [ambient air or high temperature (250°F minimum)] and (2) leakage at 1 and 4 in. of water pressure difference (8 and 12 in. of water classification optional). Smoke dampers are tested under conditions of maximum airflow. UL’s annual Fire Resistance Directory lists fire resistances of floor/roof and ceiling assemblies with and without ceiling fire dampers.

For a more detailed presentation of fire protection, see the NFPA (2008) Fire Protection Handbook, Chapter 53 of the 2019 ASHRAE Handbook—HVAC Applications, and Klote et al. (2012).

 Duct Insulation

In all new construction (except low-rise residential buildings), air-handling ducts and plenums that are part of an HVAC air distribution system should be thermally insulated in accordance with ASHRAE Standard 90.1. Duct insulation for new low-rise residential buildings should comply with ASHRAE Standard 90.2. Existing buildings should meet requirements of ASHRAE Standard 100. In all cases, thermal insulation should meet local code requirements. Insulation thicknesses in these standards are minimum values; economic and thermal considerations may justify higher insulation levels. Additional insulation, vapor retarders, or both may be required to limit vapor transmission and condensation.

Duct heat gains or losses must be known to calculate supply air quantities, supply air temperatures, and coil loads. To estimate duct heat transfer and entering or leaving air temperatures, refer to Chapters 4 and 23.

 Physical Security

Ducts entering into spaces considered secured or sensitive should contain measures to detect or inhibit forced entry into those spaces through the duct system. Inhibiting measures should be based on a delay or resistance time set by the facility owner or user. The following security measures should be considered:

  • Barrier duct bars: placement should be at locations deemed appropriate by the facility owner and user, or where secured or sensitive area boundaries exist (e.g., duct penetration through the wall of a secured room). Bar diameter, material, and spacing should be established by the facility owner or user. Ensure that barriers do not inhibit proper operation and maintenance of dampers, detectors, sensors, and other devices in the duct system.

  • Welded diffuser and return grilles: grille material and spacing should be established by the facility owner or user.

  • Sensors on access doors: sensors should be connected to a facility security system or panel, and notify security personnel of a duct system breach. Communicating HVAC maintenance schedules to security personnel is necessary to ensure that an intrusive duct system breach is not confused with HVAC system maintenance.

 Louvers

Use Figure 19 for preliminary sizing of air intake and exhaust louvers. For air quantities greater than 7000 cfm per louver, the air intake gross louver openings are based on 400 fpm; for exhaust louvers, 500 fpm is used for air quantities of 5000 cfm per louver and greater. For smaller air quantities, see Figure 19. These criteria are presented on a per-louver basis (i.e., each louver in a bank of louvers) to include each louver frame. Representative production-run louvers were used in establishing Figure 19, and all data used were based on AMCA Standard 500-L tests. For louvers larger than 16 ft2, the free areas are greater than 45%; for louvers less than 16 ft2, free areas are less than 45%. Unless specific louver data are analyzed, no louver should have a face area less than 4 ft2. If debris can collect on the screen of an intake louver, or if louvers are located at grade with adjacent pedestrian traffic, louver face velocity should not exceed 100 fpm.

Louvers require special treatment because the blade shapes, angles, and spacing cause significant variations in louver-free area and performance (pressure drop and water penetration). Selection and analysis should be based on test data obtained from the manufacturer in accordance with AMCA Standard 500-L, which presents both pressure drop and water penetration test procedures and a uniform method for calculating the free area of a louver. Tests are conducted on a 48 in. square louver with the frame mounted flush in the wall. For water penetration tests, rainfall is 4 in./h, no wind, and the water flow down the wall is 0.25 gpm per linear foot of louver width.

AMCA Standard 500-L also includes a method for measuring water rejection performance of louvers. These louvers are subjected to simulated rain and wind pressure and tested at a rainfall of 3 in./h falling on the louver’s face with a predetermined wind velocity directed at the face of the louver (typically 29.1 or 44.7 mph). Effectiveness ratings are assigned at various airflow rates through the louver.

 Duct Shape Selection

No Space Constraints. Round ductwork is preferable to rectangular or flat oval ductwork when adequate space is available for the following reasons.

  • Weight of round ductwork is less than rectangular. Figure 20 shows the relative weight of rectangular duct to round duct for duct pressures from ±0.5 to ±10 in. of water when the equivalent diameter of the rectangular duct is the same as the round duct diameter. Equivalent diameter is defined as the diameter of a rectangular duct that has equal resistance to flow for equal flow and length.

  • Perimeter of round ducts is less than rectangular ducts. For rectangular duct aspect ratios from 2 to 4, the increase is approximately 30 to 55%. This increase results in increased insulation, including possible thickness to offset the additional heat transfer. For a comprehensive study of round and rectangular ducts as they affect system performance, consult McGill (1988).

  • Round ducts have an excellent resistance to low-frequency break-out noise (Schaffer 2005).

  • Duct rumble can occur in rectangular duct systems (Paulauskis 2016).

Criteria for Louver Sizing

Figure 19. Criteria for Louver Sizing


Relative Weight of Rectangular Duct to Round Spiral Duct

Figure 20. Relative Weight of Rectangular Duct to Round Spiral Duct


Maximum Airflow of Round, Flat Oval, and Rectangular Ducts as Function of Available Ceiling Space

Figure 21. Maximum Airflow of Round, Flat Oval, and Rectangular Ducts as Function of Available Ceiling Space


Table 9 Maximum Airflow of Round, Flat Oval and Rectangular Ducts as Function of Available Ceiling Space

A. Design Criterion: 0.08 in. of water per 100 ft or 2500 fpm Maximum

Minimum Clearance for Duct, in.

18

22

26

30

34

38

Single Round Duct

  Duct diameter, in.

14

18

22

26

30

34

  Airflow, cfm

950

1900

3200

4900

7300

10,000

  Velocity, fpm

889

1075

1212

1329

1487

1586

Rectangular Duct with Aspect Ratio = 2

  Rectangular W × H, in.

28 × 14

36 × 18

44 × 22

52 × 26

60 × 30

68 × 34

  Airflow, cfm

2900

5500

9800

14,900

21,200

30,000

  Velocity, fpm

1065

1222

1458

1587

1696

1869

  Equivalent diameter De, in.

21.3

27.4

33.5

39.6

45.7

51.8

Flat Oval Duct with Aspect Ratio = 2

  Flat oval A × a, in.

28 × 14

36 × 18

44 × 22

52 × 26

60 × 30

68 × 34

  Airflow, cfm

2700

5400

9000

14,000

21,000

28,000

  Velocity, fpm

1111

1344

1500

1670

1882

1954

  Equivalent diameter De, in.

20.7

26.6

32.5

38.4

44.4

50.3

Two Round Ducts in Parallel

  Duct diameter, in.

Two 12

Two 16

Two 20

Two 24

Two 28

Two 32

  Airflow, cfm

630 each

1350 each

2450 each

3950 each

5950 each

8500 each

  Velocity, fpm

802

967

1123

1257

1391

1522

B. Design Criterion: 0.2 in. of water per 100 ft or 2500 fpm Maximum

Minimum clearance for duct, in.

18

22

26

30

34

38

Single Round Duct

  Duct diameter, in.

14

18

22

26

30

34

  Airflow, cfm

1550

3000

5100

8000

11,500

16,000

  Velocity, fpm

1450

1698

1932

2170

2343

2538

Rectangular Duct with Aspect Ratio = 2

  Rectangular W × H, in.

28 × 14

36 × 18

44 × 22

52 × 26

60 × 30

68 × 34

  Airflow, cfm

4700

9200

15,600

23,500

31,300

40,200

  Velocity, fpm

1727

2044

2321

2303

2504

2504

  Equivalent diameter De, in.

21.3

27.4

33.5

39.6

45.7

51.8

Flat Oval Duct with Aspect Ratio = 2

  Flat oval A × a, in.

28 × 14

36 × 18

44 × 22

52 × 26

60 × 30

68 × 34

  Airflow, cfm

4500

8900

15,100

21,000

27,900

35,900

  Velocity, fpm

1852

2216

2516

2506

2500

2505

  Equivalent diameter De, in.

20.7

26.6

32.5

38.4

44.4

50.3

Two Round Ducts in Parallel

  Duct diameter, in.

Two 12

Two 16

Two 20

Two 24

Two 28

Two 32

  Airflow, cfm

1030 each

2210 each

4000 each

6460 each

9700 each

13,800 each

  Velocity, fpm

1311

1583

1833

2056

2268

2471

C. Design Criterion: 0.6 in. of water per 100 ft or 3000 fpm Maximum

Minimum clearance for duct, in.

18

22

26

30

34

38

Using Single Round Duct

  Duct diameter in.

14

18

22

26

30

34

  Airflow, cfm

2750

5300

8000

11,100

14,800

19,000

  Velocity, fpm

2572

3000

3031

3011

3015

3013

Rectangular Duct with Aspect Ratio = 2

  Rectangular W × H, in.

28 × 14

36 × 18

44 × 22

52 × 26

60 × 30

68 × 34

  Airflow, cfm

8200

13,500

20,200

28,200

37,500

48,200

  Velocity, fpm

3012

3000

3005

3004

3000

3002

  Equivalent diameter De, in.

21.3

27.4

33.5

39.6

45.7

51.8

Flat Oval Duct with Aspect Ratio = 2

  Flat oval A × a, in.

28 × 14

36 × 18

44 × 22

52 × 26

60 × 30

68 × 34

  Airflow, cfm

7300

12,100

18,000

25,200

33,500

43,000

  Velocity, fpm

3004

3012

3000

3007

3002

3000

  Equivalent diameter De, in.

20.7

26.6

32.5

38.4

44.4

50.3

Two Round Ducts in Parallel

  Duct diameter, in.

Two 12

Two 16

Two 20

Two 24

Two 28

Two 32

  Airflow, cfm

1850 each

3960 each

6550 each

9430 each

12,830 each

16,800 each

  Velocity, fpm

2355

2836

3000

3000

3000

3000


Space Constraints. Space constraints and obstructions, particularly ceiling height, are frequent problems. In these cases, the choice is round, rectangular, or flat oval ducts, depending on the air quantity that needs to be conveyed by the duct. Table 9 and Figure 21 cover three design cases: 0.08, 0.2, and 0.6 in. of water per 100 ft friction rates. Friction rate 0.2 in. of water per 100 ft is at the middle range. In Table 9, six ceiling (plenum) heights ranging from 18 to 38 in., in 4 in. increments, are covered. Space allocated for insulation and reinforcement is 2 in. all around. The aspect ratio of the rectangular and flat oval ducts is 2:1. Figure 21 shows the maximum airflow as a function of the design friction rates and plenum spaces, as noted. For example, the 30 in. plenum as a design friction rate of 0.2 in. of water per 100 ft is 8000 cfm maximum for a 26 in. round duct; 23,500 cfm for a 52 × 26 in. rectangular duct; and 21,000 cfm for a 52 × 26 in. flat oval duct. The airflow capacity of two round 26 in. ducts is 6460 cfm each.

When selecting a rectangular or flat oval duct, consider the following:

  • Rectangular duct has the advantage in weight because construction standards for flat oval exist only for +10 in. of water, whereas rectangular has seven pressure classes, starting at 0.5 in. of water. All rectangular pressure classes are ±.

    Note: Negative-pressure flat oval duct systems can be designed by using +10 in. of water sheet gages with the negative-pressure rectangular reinforcement welded to the duct.

  • Low-frequency breakout noise for flat oval is good, fair for rectangular (Schaffer 2005).

  • Duct rumble can occur in rectangular duct systems (Paulauskis 2016).

  • Perimeter. Using rectangular duct instead of flat oval when sized for equivalent diameter increases the perimeter roughly 17 to 7% for aspect ratios ranging from 1 to 4, respectively. This increase results in an increased surface area. Flat oval requires less insulation. For a comprehensive study of flat oval and rectangular ducts as they affect system performance, consult McGill (1995).

  • Duct Lengths. Rectangular duct is available in 4, 5, or 6 ft lengths. Spiral round and flat oval can be provided in longer lengths.

 Testing and Balancing

Each air duct system should be tested, adjusted, and balanced. Guidance and procedures are given in Chapter 38 of the 2019 ASHRAE Handbook—HVAC Applications and in ASHRAE Standard 111. To determine fan total (or static) pressure from field measurements taking into account fan system effect, consult AMCA (2011b) Publication 203, which provides numerous fan/system configurations encountered in the field.

Many VAV noise complaints have been traced to control problems. Although most problems are associated with improper installation, many are caused by poor design. The designer should specify high-quality fans or air handlers within their optimum ranges, not at the edge of their operation ranges, where low system tolerances can lead to inaccurate fan flow capacity control. Also, in-duct static pressure sensors should be placed in duct sections having the lowest possible air turbulence (i.e., at least three equivalent duct diameters from any elbow, takeoff, transition, offset, or damper).

6.2 DESIGN RECOMMENDATIONS

  • Engage the architect and structural engineer early to coordinate shafts for systems.

  • Route ducts as straight as possible to reduce pressure loss, noise, and first costs.

  • Use round spiral ducts whenever round ducts can fit within space constraints.

  • Avoid consecutive fittings and close-coupled fittings because they can significantly increase pressure losses.

  • Use return air plenums when possible because they reduce both energy and first costs. Plenum return requires fire-rated construction.

  • Design air distribution systems to minimize flow resistance and turbulence. High flow resistance increases fan pressure, which results in higher noise being generated by the fan, especially at low frequencies. Turbulence also increases flow noise generated by duct fittings and dampers, especially at low frequencies.

  • Efficient fittings create the least turbulence and noise. Figure 22 provides generalized guidelines for minimizing regenerated noise from takeoffs. Tables 10 and 11 provide specific guidance for tees and wyes.

  • Duct transitions should not exceed an included angle of 15°.

  • To avoid fan system effects, fans should discharge into duct sections that remain straight for as long as possible, up to 10 duct diameters from the fan discharge to allow flow to fully develop (Figure 23). Use the ASHRAE Duct Fitting Database (ASHRAE 2016) to account for fan outlet system effects (SD7 and SR7-series).

  • Design duct connections at the fan inlet for uniform and straight airflow. Both turbulence and flow separation at the fan blades can significantly increase fan-generated noise. To account for fan inlet system effects, use the ASHRAE Duct Fitting Database (ASHRAE 2016) (ED7 and ER7 series).

  • For all except very-noise-sensitive applications, select VAV reheat boxes for a total pressure loss from 0.5 to 0.6 in. of water; for a fan-powered VAV box, from 0.6 to 0.7 in. of water. For details, see Taylor and Stein (2004).

  • VAV terminal unit inlet duct should be the same size as the inlet to the box, unless the box is in the critical path or the length exceeds about 15 ft from the takeoff. Duct upstream of box inlets should be rigid sheet metal duct, 4 ft minimum. Do not use flexible duct immediately upstream of VAV boxes.

  • See Figure 24 for Schaffer’s (2005) guidelines for the installation of single-duct, dual-duct, and induction terminal units, as well as parallel and series flow fan-powered units.

  • Place fan-powered mixing boxes away from noise-sensitive areas.

  • Use demand-based static pressure set-point reset to reduce fan energy and noise.

  • For constant-volume systems, select the fan to operate as near as possible to its rated peak efficiency. Also, select a fan that generates the lowest possible noise at required design conditions. Using an oversized or undersized fan that does not operate at or near rated peak efficiency can substantially increase noise levels. For VAV applications, see Schaffer (2005).

Commentary. Consult Noise and Vibration Control for HVAC Systems (Schaffer 2005) for the following guidelines related to duct systems:

  • Selection of mechanical room walls

  • Noise control for mechanical rooms

  • Upward noise control for mechanical rooms

  • Duct penetrations through walls

  • Structural support of rooftop equipment for vibration control

Guidelines For Minimizing Regenerated Noise in Takeoff (Schaffer 2005)

Figure 22. Guidelines For Minimizing Regenerated Noise in Takeoff (Schaffer 2005)


Guidelines for Centrifugal Fan Installations (Schaffer 2005)

Figure 23. Guidelines for Centrifugal Fan Installations (Schaffer 2005)


Guidelines for VAV Terminal Unit Installation (Schaffer 2005)

Figure 24. Guidelines for VAV Terminal Unit Installation (Schaffer 2005)


Table 10 Options for Selecting 90° Takeoff

Code

Description

Efficiency

Loss Coefficient

Maina

Branchb

SD5-12

Tee, 45° entry branch

Highest

0.15

0.64

SD5-4

Wye, 45°, Straight body branch with 45° elbow, 90° to main

0.15

0.74

SD5-11

Tee, Conical branch

0.15

0.87

SD5-10

Tee, Conical branch tapered into body

0.15

1.10

SD5-9

Tee

Lowest

0.15

1.80

a Qs/Qc = 0.8; As/Ac = 0.69

b Qb/Qc = 0.2; Ab/Ac = 0.25



Table 11 Options for Selecting 45° Takeoff (Wye)

Code

Description

Efficiency

Loss Coefficient

Main, Csa

Branch, Cbb

SD5-2

Wye, 45°, Conical branch tapered into body

Highest

0.15

0.45

SD5-3

Wye, 45°, Straight body branch with reduction transition

0.15

0.50

SD5-1

Wye, 45°

Lowest

0.15

0.70

a Qs/Qc = 0.8; As/Ac = 0.69

b Qb/Qc = 0.2; Ab/Ac = 0.25


6.3 DESIGN METHODS

Equal Friction Method. The equal friction method for sizing duct systems uses a constant friction rate. The target velocity determines the size of the first duct section both downstream and upstream of the fan. From the size determined by the target velocity, the design friction rate is determined to size all remaining duct sections except for connections to VAV and constant-volume (CV) terminal units and diffusers in the critical path, or for sections whose length exceeds around 15 ft. In these cases, the inlet to terminal units should have at least three diameters of rigid duct and 6 ft maximum of rigid or flexible duct (see Figure 9) to diffusers. The section upstream of the rigid duct to terminal units and the section of rigid/flexible duct to diffusers should be sized by the design friction rate, and an appropriate transition placed between sections. Refer to sections 8 and 9 in Figure 26 for an example.

Static Regain Method. The static regain method uses the conservation of momentum principle, which results in an increase in static pressure when the velocity is reduced in an airstream. This method sizes the main and branch ducts after a junction so that the recovery in static pressure caused by the reduced velocity is approximately equal to the total pressure drop caused by the duct and fittings in the subject duct section according to Equation (41). This is done iteratively by selecting a size for a section and checking to see if the section’s static pressure loss is close to zero. The basic steps are to design the first section at the velocity recommended in Table 12. Then each downstream section is subsequently sized using the same duct size as the upstream section as a starting point. If there is no static regain, meaning there is a positive static pressure loss, then the downstream section will be the same size as the upstream section. But, if there is static regain, meaning the change in static pressure is negative, then an opportunity exists to use a smaller duct section. Typically, the next smaller size available that is smaller than the upstream section is selected and the calculations are repeated. Refer to column 12 of Table 15 for examples of static regain.


Table 12 Recommended Maximum Airflow Velocities to Achieve Specified Acoustic Design Criteria*

Duct Location

NC or RC Rating in Adjoining Occupancy

Maximum Airflow Velocity, fpm

Rectangular Duct

Round Duct

1

2

3

4

In shaft or above solid drywall ceiling

45

3500

5000

35

2500

3500

25 or less

1500

2500

Above suspended acoustical ceiling

45

2500

4500

35

1750

3000

25 or less

1000

2000

Duct within occupied space

45

2000

3900

35

1450

2600

25 or less

950

1700


For connections to VAV and CV terminal units and diffusers in the critical path or the section length with the terminal unit or diffuser exceeds around 15 ft, the inlet to terminal units should have at least three diameters of rigid duct and 6 ft maximum of rigid or flexible duct (see Figure 6) to diffusers. The section upstream of the rigid duct to terminal units and the section of rigid/flexible duct to diffusers should be sized by the static regain method and an appropriate transition placed between sections. Refer to sections 8 and 9 in Figure 26 for an example.

(40)

Rearranging,

(41)

where

pv1 = velocity pressure at section 1, in. of water
pv2 = velocity pressure atsection 2, in. of water
Δpt,1–2 = total pressure loss from section 1 to 2, in. of water
Δps,1–2 = static pressure regain (+) or loss (–), in. of water

Balancing. When system unbalance is greater than about 30%, it is recommended that balance be improved by changing duct size, and/or fittings from a select few that have comparable efficiency without introducing additional significant turbulence (noise). Tables 10 and 11 are examples.

 Noise Control

Understanding what noise is and how to control it is fundamental to duct design. The underlying principles of sound and vibration are covered in Chapter 8. Chapter 48 of the 2019 ASHRAE Handbook—HVAC Applications contains technical discussions and design examples helpful to the design engineer. AHRI Standard 885 has procedures for estimating sound pressure levels in the occupied zone for the portion of the system downstream of terminal units. For guidance in designing HVAC systems to avoid noise and vibration problems, consult Schaffer (2005). Specifying quiet equipment and designing systems to avoid noise and vibration problems are necessary parts of the design process.

Noise in system comes from fans and generated noise resulting from air turbulence in ducts, individual fittings, close-coupled fittings, dampers, air modulating equipment and diffusers/grilles. Objectionable self-generated duct noise can be controlled by limiting the duct velocity to the values listed in Table 12.

 Goals

The goal of duct design is an air distribution system without objectionable noise and minimum life-cycle cost (LCC). Noise can be controlled by limiting the duct velocity to the values listed in Table 12. For example, for ductwork above a suspended acoustical ceiling and with a maximum allowable NC or RC of 35 in the adjoining space, the maximum round and rectangular duct airflow velocities are 3000 and 1750 fpm, respectively. Use this velocity to size the first duct section either upstream or downstream from the fan for all duct design methods. Lowering duct velocity reduces system operating cost and minimizes noise from sources other than ducts (fittings, close-coupled fittings, and dampers).

Commentary: In 1988, Dr. Robert J. Tsal developed the T-method (Tsal and Adler 1987; Tsal et al. 1988, 1990) to design systems with a minimum LCC. The T-method was technically sound, but the system cost was not sufficiently accurate. As a result, the T-method was removed from the Handbook in 2013.

 Design Method to Use

Supply Duct Sizing.

  • Size fan supply ducts by either the equal friction (EF) or static regain (SR) method. The duct velocity anywhere in the system should not exceed the velocity listed in Table 12.

  • Size ducts downstream of terminal boxes, toilet exhaust ducts, and other low-pressure systems (e.g., in Figure 25C) using the equal friction method with a friction rate in the range from 0.05 to 0.20 in. of water per 100 ft such that the duct velocity in the duct anywhere in the system does not exceed the values in Table 12. Use Table 13 as a guide to select the design friction rate.

  • Terminal unit (VAV box) runouts should be full size with the exception that runouts in the “critical” path or a runout length greater than about 15 ft should be a minimum 5 ft of rigid duct full size and the remainder’s size determined by the design method (e.g., Example 8 and Figure 26).

  • Diffuser runouts should be full size, except for runouts in the critical path or a runout length greater than about 15 ft: these runouts should be at least 6 ft of flexible-duct full size, and the remainder’s size determined by the design method.

Table 13 Guide for Selecting Low-Pressure System Friction Rate*

Airflow

Q, cfm

in. of water per 100 ft

0.05

0.10

0.12

0.15

0.20

D, in.

V, fpm

D, in.

V, fpm

D, in.

V, fpm

D, in.

V, fpm

D, in.

V, fpm

500

13

542

11

758

11

758

10

917

10

917

1,000

16

716

14

935

14

935

13

1085

12

1273

2,000

21

832

18

1132

18

1132

17

1269

16

1432

3,000

24

955

21

1247

20

1375

20

1375

18

1698

4,000

27

1006

24

1273

23

1386

22

1515

21

1663

5,000

29

1090

26

1356

25

1467

24

1592

22

1894

10,000

38

1270

33

1684

32

1790

31

1908

29

2180

15,000

44

1421

39

1808

37

2009

36

2122

34

2379

20,000

49

1527

43

1983

42

2079

40

2292

38

2539

25,000

54

1572

47

2075

45

2264

43

2479

41

2727

30,000

58

1635

50

2200

48

2387

46

2599

44

2841

* Table developed using ASHRAE Duct Fitting Database (ASHRAE 2016): CD11-4 (ε = 0.0004 ft; ρ = 0.075 lbm/ft3).


Return Duct Systems.

  • Sizing ducted returns depend on economizer relief system. For systems with return fans (Figure 25A), the return air ducts are sized using the EF method. The SR method does not work for negative-pressure duct systems.

    If building relief is by relief fans or gravity/motorized dampers, pressure drop should be kept low as shown by the total pressure grade line associated with Figures 25B and 25C.

    Control dampers in the economizer system should be selected (parallel or opposed blade) and sized in compliance with ASHRAE Guideline 16. Louvers should be sized in accordance with the section on Louvers, under Duct Design.

  • Unducted return air shafts are typically sized for low pressure loss using either a fixed friction rate, velocity, or both. Typically, shafts are simply sized based on velocity. Maximum velocities are generally in the 800 to 1200 fpm range through the free area at the top of the shaft (highest airflow rate).

  • Diffuser/grille runouts should be designed by the design method of choice and a transition located at the outlet. For outlets in the critical path, the outlet duct size should be increased. Registers should not be used because of the damper.

Example 8.

For the VAV system shown in Figure 26, design the duct system by both the equal friction (EF) and static regain (SR) methods, and compare the section duct sizes, total pressure required for each path, and the unbalance between paths.

The system is located in Denver (5430 ft elevation) and the duct is spiral round, galvanized steel (absolute roughness ε = 0.0004 ft). The duct system is located above a suspended acoustical ceiling, and the allowable background sound in the occupied spaces is NC-35. Terminals T1, T2, T3, and T4 (VAV boxes with a one-row hot-water coil) are 800 cfm. VAV box loss coefficients are 1.68.

Solution: Use the ASHRAE Duct Fitting Database (ASHRAE 2016) to determine the air density, which is used to identify the velocity pressure and fitting loss coefficients for fittings. Density is 0.061 lbm/ft3 (Figure 27). The maximum design duct velocity from Table 12 is 3000 fpm. The EF and SR calculations are shown by Tables 14 and 15 spread-sheets.

For both the EF and SR designs, the duct size for section 2 is 14 in. determined using CD11-3 (Figure 28). Sizing the remaining section depends on the design method. For the equal friction design method, the system equal friction (also from CD11-3) is 0.67 in. of water per 100 ft. Knowing the system design friction rate, the duct sizes are determined by CD11-4. Figure 29 is an example for Section 4. For the static regain method, all sections other than the terminal unit runouts are sized by iterating using Equation (41) (column 12 on the spreadsheet). For example, the results of the iteration for section 4 are summarized by Table 16. The solution is the diameter that gives the result from Equation (41) that is closest to zero: in this case, 13 in.

Tables 17 and 18 summarize the results. The SR design is slightly better balanced, 18% compared to 23%, and the SR design requires 9% less energy. In addition, the SR sizes are slightly larger, and thus potentially less noisy. Both methods have static regain, but the SR design uses the regain more efficiently.


Economizer Duct System Shown (ASHRAE Guideline 16)

Figure 25. Economizer Duct System Shown (ASHRAE Guideline 16)


Table 14 Example 8, Equal Friction Design



Table 15 Example 8, Static Regain Design


System Layout for Example 8

Figure 26. System Layout for Example 8


Air Density for Example 8 ASHRAE Duct Fitting Database (ASHRAE 2016)

Figure 27. Air Density for Example 8 ASHRAE Duct Fitting Database (ASHRAE 2016)


Sizing Section 2 for EF and SR Design Examples

Figure 28. Sizing section 2 for EF and SR Design Examples


6.4 INDUSTRIAL EXHAUST SYSTEMS

Chapter 32 of the 2019 ASHRAE Handbook—HVAC Applications discusses design criteria, including hood design, for industrial exhaust systems. Exhaust systems conveying vapors, gases, and smoke are designed by the equal-friction method. Systems conveying particulates are designed by the constant velocity method at duct velocities adequate to convey particles to the system air cleaner. For contaminant transport velocities, see Table 2 in Chapter 32 of the 2019 ASHRAE Handbook—HVAC Applications.

EF Design: Sizing Sections 4, 6, and 8 Knowing Design Friction Rate (Section 4 Shown)

Figure 29. EF Design: Sizing Sections 4, 6, and 8 Knowing Design Friction Rate (Section 4 Shown)



Table 16 Static Regain Iteration Process for section 4

Iteration

Calculation

Duct Size, in.

(pv1pv2) – Δpi

Remarks

1

4a

14

0.08

 

2

4b

13

−0.05

Solution



Table 17 Summary of System Duct Sizes

Section

Size, in.

Remarks

EF

SR

1

18 × 20

18 × 20

Fan outlet

2

14

14

Initial section

4

13

13

Sections affected by design method

6

11

12

8

9

10

3

8

8

Terminal runout

5

8

8

Terminal runout

7

8

8

Terminal runout

9

8

8

Terminal runout



Table 18 System Unbalance

Path

Equal Friction

Static Regain

Pt, in. of water

Unbalance

Pt, in. of water

Unbalance

A

0.88

23%

0.88

18%

B

0.95

17%

0.95

11%

C

1.08

6%

1.00

7%

D

1.15

0%

1.07

0%


Two pressure-balancing methods can be considered when designing industrial exhaust systems. One method uses balancing devices (e.g., dampers, blast gates) to obtain design airflow through each hood. The other approach balances systems by adding resistance to ductwork sections (i.e., changing duct size, selecting different fittings, increasing airflow). This self-balancing method is preferred, especially for systems conveying abrasive materials. Where potentially explosive or radioactive materials are conveyed, the prebalanced system is mandatory because contaminants could accumulate at the balancing devices. To balance systems by increasing airflow, use Equation (42), which assumes that all ductwork has the same diameter and that fitting loss coefficients, including main and branch tee coefficients, are constant.

(42)

where

Qc = airflow rate required to increase Pl to Ph, cfm
Qd = total airflow rate through low-resistance duct run, cfm
Ph = absolute value of pressure loss in high-resistance ductwork section(s), in. of water
Pl = absolute value of pressure loss in low-resistance ductwork section(s), in. of water

For systems conveying particulates, use elbows with a large centerline radius-to-diameter ratio (r/D), greater than 1.5 whenever possible. If r/D is 1.5 or less, abrasion in dust-handling systems can reduce the life of elbows. Elbows are often made of seven or more gores, especially in large diameters. For converging flow fittings, a 30° entry angle is recommended to minimize energy losses and abrasion in dust-handling systems. For the entry loss coefficients of hoods and equipment for specific operations, see Chapter 32 of the 2019 ASHRAE Handbook—HVAC Applications and ACGIH (2016).

Commentary: Fitting CD11-5 of the ASHRAE Duct Fitting Database (ASHRAE 2016) is available for sizing minimum-velocity ducts conveying particulates.

Metalworking Exhaust System for Example 9

Figure 30. Metalworking Exhaust System for Example 9


Example 9.

For the metalworking exhaust system in Figures 30 and 31, size the ductwork and calculate fan static pressure requirement for an industrial exhaust designed to convey granular materials. Pressure-balance the system by changing duct sizes and adjusting airflow rates. Minimum particulate transport velocity for the chipping and grinding table ducts (sections 1 and 5, Figure 31) is 4000 fpm. For ducts associated with the grinder wheels (sections 2, 3, 4, and 5), minimum duct velocity is 4500 fpm. Ductwork is galvanized steel, with absolute roughness of 0.0003 ft. Assume that air is standard and that duct and fittings are available in the following sizes: 3 to 9.5 in. diameters in 0.5 in. increments, 10 to 37 in. diameters in 1 in. increments, and 38 to 90 in. diameters in 2 in. increments.

The building is one story, and the design wind velocity is 20 mph. For the stack, use design J shown in Figure 2 in Chapter 45 of the 2019 ASHRAE Handbook—HVAC Applications for complete rain protection; stack height, determined by calculations from Chapter 45, is 16 ft above the roof. This height is based on minimized stack downwash; therefore, the stack discharge velocity must exceed 1.5 times the design wind velocity.

Solution: The following table summarizes initial duct sizes and transport velocities for contaminated ducts upstream of the collector. The 4474 fpm velocity in sections 2 and 3 is acceptable because the transport velocity is not significantly lower than 4500 fpm. For the next available duct size (4.5 in. diameter), the duct velocity is 5523 fpm, significantly higher than 4500 fpm.

Duct Section

Design Airflow, cfm

Transport Velocity, fpm

Duct Diameter, in.

Duct Velocity, fpm

1

1800

4000

9

4074

2, 3

610 each

4500

5

4474

4

1220

4500

7

4565

5

3020

4500

11

4576

Design calculations up through the junction after sections 1 and 4 are summarized as follows:


Design No.

D1, in.

Δp1, in. of water

Δp2+4, in. of water

Imbalance, Δp1 – Δp2+4

1

9

1.46

3.09

1.63

2

8.5

2.00

3.08

−1.08

3

8

2.79

3.00

−0.21

4

7.5

3.92

2.88

+1.04

Q1 = 1800 cfm

Q2 = 610 cfm; D2 = 5 in. dia.

Q3 = 610 cfm; D3 = 5 in. dia.

Q4 = 1220 cfm; D4 = 7 in. dia.


For (initial) design 1, the imbalance between section 1 and section 2 (or 3) is 1.63 in. of water, with section 1 requiring additional resistance. Decreasing section 1 duct diameter by 0.5 in. increments results in the least imbalance, 0.21 in. of water, when the duct diameter is 8 in. (design 3). Because section 1 requires additional resistance, estimate the new airflow rate using Equation (42):

At 1870 cfm flow in section 1, 0.13 in. of water imbalance remains at the junction of sections 1 and 4. By trial-and-error solution, balance is attained when the flow in section 1 is 1850 cfm. The duct between the collector and fan inlet is 13 in. round to match the fan inlet (12.75 in. diameter). To minimize downwash, the stack discharge velocity must exceed 2640 fpm, 1.5 times the design wind velocity (20 mph) as stated in the problem definition. Therefore, the stack is 14 in. round, and the stack discharge velocity is 2872 fpm.

Table 19 summarizes the system losses by sections. The straight duct friction factor and pressure loss were calculated by Equations (18) and (19). Table 20 lists fitting loss coefficients and input parameters necessary to determine the loss coefficients. The fitting loss coefficients are from the ASHRAE Duct Fitting Database. Figure 32 shows a pressure grade line of the system. Fan total pressure, calculated by Equation (15), is 7.89 in. of water. To calculate the fan static pressure, use Equation (17):

where 0.81 in. of water is the fan outlet velocity pressure. The fan airflow rate is 3070 cfm, and its outlet area is 0.853 ft3 (10.125 by 12.125 in.). Therefore, the fan outlet velocity is 3600 fpm.

System Schematic with Section Numbers for Example 9

Figure 31. System Schematic with Section Numbers for Example 9


Table 19 Total Pressure Loss Calculations by Sections for Example 9

Duct Sectiona

Duct Element

Airflow, cfm

Duct Size. in. ϕ

Velocity, fpm

Velocity Pressure, in. of water

Duct Length,bft

Summary of Fitting Loss Coefficientsc

Duct Pressure Loss/100 ft, in. of waterd

Total Pressure Loss, in. of water

Section Pressure Loss, in. of water

1

Duct

1850

8

5300

23.7

4.64

1.10

 
 

Fittings

1850

 

5300

1.75

1.07

1.87

2.97

2, 3

Duct

610

5

4474

8.5

5.96

0.51

 
 

Fittings

610

 

4474

1.25

1.06

1.33

1.84

4

Duct

1220

7

4565

11.5

4.09

0.47

 
 

Fittings

1220

 

4565

1.30

0.51

0.66

1.13

5

Duct

3070

11

4652

8.5

2.44

0.21

 
 

Fittings

3070

 

4652

1.35

0.22

0.30

0.51

Collector,e fabric

3070

3.0

3.0

6

Duct

3070

13

3331

10.5

1.05

0.11

 
 

Fittings

3070

 

3331

0.69

0.03

0.02

0.13

7

Duct

3070

14

2872

50

0.72

0.36

 
 

Fittings

3070

 

2872

0.51

1.80

0.92

1.28

a See Figure 29.

b Duct lengths are to fitting centerlines.

c See Table 20.

d Duct pressure based on a 0.0003 ft absolute roughness factor.

e Collector manufacturers set fabric bag cleaning mechanism to actuate at a pressure difference of 3.0 in. of water between inlet and outlet plenums. Pressure difference across clean media is approximately 1.5 in. of water.



Table 20 Loss Coefficient Summary by Sections for Example 9

Duct Section

Fitting Number

Type of Fitting

ASHRAE Fitting No.a

Parameters

Loss Coefficient

1

1

Hoodb

Hood face area: 3 by 4 ft

0.25

 

2

Elbow

CD3-10

90°, 7 gore, r/D = 2.5

0.11

 

4

Capped wye (45°), with 45° elbow

ED5-6

Ab/Ac = 1

0.61 (Cb)

 

5

Wye (30°), main

ED5-1

Qs/Qc = 0.60, As/Ac = 0.529, Ab/Ac = 0.405

0.10 (Cs)

 

Summation of Section 1 loss coefficients

1.07

2,3

6

Hoodc

Type hood: For double wheels, dia. = 22 in. each, wheel width = 4 in. each; type takeoff: tapered

0.40

 

7

Elbow

CD3-12

90°, 3 gore, r/D = 1.5

0.34

 

8

Symmetrical wye (60°)

ED5-9

Qb/Qc = 0.5, Ab1/Ac = 0.51, Ab2/Ac = 0.51

0.32 (Cb)

 

Summation of Section 2 and 3 loss coefficients

 

1.06

4

9

Elbow

CD3-10

90°, 7 gore, r/D = 2.5

0.11

 

10

Elbow

CD3-13

60°, 3 gore, r/D = 1.5

0.19

 

5

Wye (30°), branch

ED5-1

Qb/Qc = 0.40, As/Ac = 0.529, Ab/Ac = 0.405

0.21 (Cb)

 

Summation of Section 4 loss coefficients

 

0.51

5

11

Exit, conical diffuser to collector

ED2-1

L = 24 in., L/Do = 2.0, A1/Ao16

0.22

 

Summation of Section 5 loss coefficients

 

0.22

6

12

Entry, bellmouth from collector

ER2-1

r/D1 = 0.23, r = 3 in., Co = 3.30

0.03 (C1)

 

Summation of Section 6 loss coefficients

 

0.03

7

13

Diffuser, fan outlet d

SD4-2

Fan outlet size: 10.125 by 12.125 in.; L = 18 in.

0.19

 

14

Capped wye (45°), with 45° elbow

ED5-6

Ab/Ac = 1

0.61 (Cb)

 

15

Stackhead

SD2-6

De/D = 1

1.00

 

Summation of Section 7 loss coefficients

 

1.80

a From ASHRAE Duct Fitting Database.

b From Industrial Ventilation (ACGIH 2016, Figure VS-80-19).

c From Industrial Ventilation (ACGIH 2016, Figure VS-80-11).

d Fan specified: Industrial exhauster for granular materials: 21 in. wheel diameter, 12.75 in. inlet diameter, 10.125 by 12.125 in. outlet, 7.5 hp motor.


Total Pressure Grade Line for Example 9

Figure 32. Total Pressure Grade Line for Example 9


Hood suction for the chipping and grinding table hood is 2.2 in. of water, calculated by Equation (5) from Chapter 32 of the 2019 ASHRAE Handbook—HVAC Applications [Ps,h = (1 + 0.25) (1.74) = 2.2 in. of water, where 0.25 is hood entry loss coefficient Co, and 1.74 is duct velocity pressure Pv a few diameters downstream from the hood]. Similarly, hood suction for each grinder wheel is 1.7 in. of water.

where 0.4 is the hood entry loss coefficient, and 1.24 in. of water is the duct velocity pressure.


REFERENCES

ASHRAE members can access ASHRAE Journal articles and ASHRAE research project final reports at technologyportal.ashrae.org. Articles and reports are also available for purchase by nonmembers in the online ASHRAE Bookstore at www.ashrae.org/bookstore.

Abushakra, B., I.S. Walker, and M.H. Sherman. 2004. Compression effects on pressure loss in flexible HVAC ducts. International Journal of HVAC&R Research (now Science and Technology for the Built Environment) 10(3):275-289.

ACCA. 2014. Manual D—Residential duct systems. Air Conditioning Contractors of America, Washington, DC.

ACGIH. 2016. Industrial ventilation: A manual of recommended practice for design, 29th ed. American Conference of Governmental Industrial Hygienists, Lansing, MI.

AHRI. 2008. Procedure for estimating occupied space sound levels in the application of air terminals and air outlets. Standard 885-2008 with Addendum 1. Air-Conditioning, Heating, and Refrigeration Institute, Arlington, VA.

AMCA. 2011a. Fans and systems. AMCA Publication 201-02 (R2011). Air Movement and Control Association International, Arlington Heights, IL.

AMCA. 2011b. Field performance measurement of fan systems. AMCA Publication 203-90 (R2011). Air Movement and Control Association International, Arlington Heights, IL.

AMCA. 2016. Laboratory methods for testing fans for certified aerodynamic performance rating. ANSI/AMCA Standard 210-16. Also ANSI/ASHRAE/AMCA Standard 51-16.

AMCA. 2012. Laboratory methods of testing dampers for rating. ANSI/AMCA Standard 500-D-12. Air Movement and Control Association International, Arlington Heights, IL.

AMCA. 2015. Laboratory method of testing louvers for rating. ANSI/AMCA Standard 500-L-12 (R2015). Air Movement and Control Association International, Arlington Heights, IL.

AMCA. 2013. Certified ratings program—Product rating manual for air control. AMCA Publication 511-10 (Rev. 2013). Air Movement and Control Association International, Arlington Heights, IL.

ASHRAE. 2016. ASHRAE duct fitting database, v. 6.00.05.10.

ASHRAE. 2016. Energy standard for buildings except low-rise residential buildings. ANSI/ASHRAE/IES Standard 90.1-2016.

ASHRAE. 2007. Energy-efficient design of low-rise residential buildings. ANSI/ASHRAE Standard 90.2-2007.

ASHRAE. 2015. Energy conservation in existing buildings. ANSI/ASHRAE/IES Standard 100-2015.

ASHRAE. 2008. Measurement, testing, adjusting and balancing of building heating, ventilation and air-conditioning systems. ANSI/ASHRAE Standard 111-2008.

ASHRAE. 2016. Method of testing HVAC air ducts and fittings. ANSI/ASHRAE/SMACNA Standard 126-2016.

ASHRAE. 2016. Methods of testing air terminal units. ANSI/ASHRAE Standard 130-2016.

ASHRAE. In development. Method of test to determine leakage of operating HVAC air distribution systems. ANSI/ASHRAE Proposed Standard 215.

ASHRAE. 2014. Selecting outdoor, return, and relief dampers for air-side economizer systems. ASHRAE Guideline 16-2014.

Behls, H.F. 1971. Computerized calculation of duct friction. Building Science Series 39, p. 363. National Institute of Standards and Technology, Gaithersburg, MD.

Brown, R.B. 1973. Experimental determinations of fan system effect factors. In Fans and systems, ASHRAE Symposium Bulletin LO-73-1, Louisville, KY (June).

Clarke, M.S., J.T. Barnhart, F.J. Bubsey, and E. Neitzel. 1978. The effects of system connections on fan performance. ASHRAE Transactions 84(2): 227-263.

Colebrook, C.F. 1938–1939. Turbulent flow in pipes, with particular reference to the transition region between the smooth and rough pipe laws. Journal of the Institution of Civil Engineers 11:133.

Culp, C.H. 2011. HVAC flexible duct pressure loss measurements. ASHRAE Research Project RP-1333, Final Report.

Farquhar, H.F. 1973. System effect values for fans. In Fans and systems, ASHRAE Symposium Bulletin LO-73-1, Louisville, KY (June).

Griggs, E.I., and F. Khodabakhsh-Sharifabad. 1992. Flow characteristics in rectangular ducts. ASHRAE Transactions 98(1):116-127.

Griggs, E.I., W.B. Swim, and G.H. Henderson. 1987. Resistance to flow of round galvanized ducts. ASHRAE Transactions 93(1):3-16.

Heyt, J.W., and M.J. Diaz. 1975. Pressure drop in flat-oval spiral air duct. ASHRAE Transactions 81(2):221-232.

Huebscher, R.G. 1948. Friction equivalents for round, square and rectangular ducts. ASHVE Transactions 54:101-118.

Hutchinson, F.W. 1953. Friction losses in round aluminum ducts. ASHVE Transactions 59:127-138.

Idelchik, I.E., M.O. Steinberg, G.R. Malyavskaya, and O.G. Martynenko. 1994. Handbook of hydraulic resistance, 3rd ed. CRC Press/Begell House, Boca Raton.

Jones, C.D. 1979. Friction factor and roughness of United Sheet Metal Company spiral duct. United Sheet Metal, Division of United McGill Corp., Westerville, OH (August). Based on data in Friction loss tests, United Sheet Metal Company Spiral Duct, Ohio State University Engineering Experiment Station, File T-1011, September 1958.

Klote, J.H., J.A. Milke, P.G. Tumbull, A. Kashef, and M.J. Ferreira. 2012. Handbook of smoke control engineering. ASHRAE.

Kulkarni, D., S. Khaire, and S. Idem. 2009. Pressure loss of corrugated spiral duct. ASHRAE Transactions 115(1).

Madison, R.D., and W.R. Elliot. 1946. Friction charts for gases including correction for temperature, viscosity and pipe roughness. ASHVE Journal (October).

McGill. 1988. Round vs. rectangular duct. Engineering Report 147, United McGill Corp. (contact McGill Airflow Technical Service Department), Westerville, OH.

McGill. 1995. Flat oval vs. rectangular duct. Engineering Report 150, United McGill Corp. (contact McGill Airflow Technical Service Department), Westerville, OH.

Meyer, M.L. 1973. A new concept: The fan system effect factor. In Fans and Systems, ASHRAE Symposium Bulletin LO-73-1, Louisville, KY (June).

Moody, L.F. 1944. Friction factors for pipe flow. ASME Transactions 66: 671.

NFPA. 2008. Fire protection handbook, 20th ed. National Fire Protection Association. Quincy, MA.

NFPA. 2015. Installation of air-conditioning and ventilating systems. ANSI/NFPA Standard 90A. National Fire Protection Association, Quincy, MA.

Osborne, W.C. 1966. Fans. Pergamon, London.

Paulauskis, J.A. 2016. Understanding duct rumble. ASHRAE Journal 58(12):40-45.

Schaffer, M.E. 2005. A practical guide to noise and vibration control for HVAC systems, 2nd ed. ASHRAE.

Swim, W.B. 1978. Flow losses in rectangular ducts lined with fiberglass. ASHRAE Transactions 84(2):216.

Swim, W.B. 1982. Friction factor and roughness for airflow in plastic pipe. ASHRAE Transactions 88(1):269.

Taylor. S.J., and J. Stein. 2004. Sizing VAV boxes. ASHRAE Journal 46(3): 30-35.

Tsal, R.J., and M.S. Adler. 1987. Evaluation of numerical methods for ductwork and pipeline optimization. ASHRAE Transactions 93(1):17-34.

Tsal, R.J., H.F. Behls, and R. Mangel. 1988. T-method duct design, part I: Optimization theory; Part II: Calculation procedure and economic analysis. ASHRAE Transactions 94(2):90-111.

Tsal, R.J., H.F. Behls, and R. Mangel. 1990. T-method duct design, part III: Simulation. ASHRAE Transactions 96(2).

UL. Published annually. Building materials directory. Underwriters Laboratories, Northbrook, IL.

UL. Published annually. Fire resistance directory. Underwriters Laboratories, Northbrook, IL.

UL. 2013. Fire dampers. ANSI/UL Standard 555, 7th ed. Underwriters Laboratories, Northbrook, IL.

UL. 2014. Smoke dampers. ANSI/UL Standard 555S, 5th ed. Underwriters Laboratories, Northbrook, IL.

Wright, D.K., Jr. 1945. A new friction chart for round ducts. ASHVE Transactions 51:303-316.

BIBLIOGRAPHY

Abushakra, B., I.S. Walker, and M.H. Sherman. 2002. A study of pressure losses in residential air distribution systems. Proceedings of the ACEEE Summer Study 2002, American Council for an Energy Efficient Economy, Washington, D.C. LBNL Report 49700. Lawrence Berkeley National Laboratory, CA.

Carrié, F.R., J. Andersson, and P. Wouters. 1999. Improving ductwork—A time for tighter air distribution systems. Air Infiltration and Ventilation Centre, Coventry, U.K.

Hyderman, M., S. Taylor, and J. Stein. 2009. Advanced variable air volume VAV systems design guide, 3rd edition. Pacific Gas and Electric Company.



The preparation of this chapter is assigned to TC 5.2, Duct Design.