Commercial
Duct Design
Principles
Methods
Applications
ENGINEERING
TRAINING
Technical Development Program
TOP-30 791-48
(Supersedes 7200-25) (Supersedes 791-125)This Technical Development Program (TDP) is designed to stand alone as a module of training. If
desired, this text may be used in conjunetion with the PowerPoint presentation TDP-39PP (Cat. No
793-446) and the Duct Calculator (Cat, No. 794-036) or with Carrier's Duct Design software
program, When properly combined with other TDP modules, this training program is one
component of a coordinated course of study of HVAC system design.
A systems approach to learning about our business makes the most sense of any because both
engineers and designers deal with equipment in the context of operating systems within a building.
Please consult the Packaged Training Programs Catalog to see how Commercial Duet Design fits
within a total curriculum of system design.
Training Program Objectives
This TDP will provide the student with the skills and knowledge necessary to:
Understand fundamental principles and theory of airflow through duct systems.
Calculate air velocity in round and rectangular duets.
Size supply and return air duct systems using the equal friction and static regain methods.
Calculate the approximate total duct system static pressure losses requited in order to size a fan
system,
Calculate friction losses of new and existing duct systems.
Verify that an existing duct system is adequate to handle an increased airflow quantity after
system upgrades.
‘Those who wish to build their knowledge in air system duct design should consider the following
related publications for their library.
Carrier Systems Design Manual if 2 (510-308) — Air Distribution
TDP-11 (791-418), Duct Sizing Using The Duct Calculator
200-11 (794-036), Duct Calculator
7200-07 (791-007), Air Side
'7200-24B (791-224), Room Air Distribution
Catrier Duct Design Software
Important — We have dozens of engineering and system
design training materials which cover theory through
application. For a FREE Packaged Training Programs
Catalog, call (800) 962-9212COMMERCIAL DUCT DESIGN
TABLE OF CONTENTS
INTRODUCTION ,.
DUCT DESIGN CRITERIA.
CLASSIFICATIONS OF DUCT SYSTEMS......
DUCT DIMENSIONS... os
FUNDAMENTALS OF AIR DUCT DESIGN
Fan and Air Distribution System Components...
‘The Law of Conservation of Energy
Air Flow through Terminals.
Friction Losses in Ducts.
Example 1 — Using the Friction Loss Chart.
Velocity Pressure Conversion Line...
Fitting Losses...
Example 2 — Fitting Loss Calculatio
Friction Losses in Straight Duct...
Example 3 ~ Material Roughness Correction
Round vs, Rectangular Duct of Equal Friction Rate.
Round Ducts of Equal Velocity and Equal Area...
Example 4 ~ Converting from Round to Equivalent Rectangular Ducts.
Other Pressure Losses
Fan Outlet Static Pressure Loss or Gain
System Effect. om
Wind and Stack Effects...
STEPS REQUIRED TO DESIGN AN AIR DUCT SYSTEM
DUCT SIZING METHODS...
EQUAL FRICTION DUCT DESIGN PROCEDURE...
MODIFIED EQUAL FRICTION DUCT DESIGN PROCEDURE.
STATIC REGAIN DUCT DESIGN PROCEDURE.....
QUIZ I INTRODUCTION
QUIZ Il- DUCT SIZING...
WORK SESSION I.
Equal Friction Duet Design.WORK SESSION IL..
Static Regain Duct Design ..
‘APPENDIX. enn
Chart | ~ Frietion Loss Chart for Round Duct...
Table 1— Circular Equivalent Diameter, Equivalent Area, and Duct Clas of Retangulat Duets
for Equal Friction... A
‘Table 2— Recommended Maximum Duct Velocities for Low Velocity Systems (FPM)
Table 3 ~ Velocity Pressures...
‘Table 4 — Duct Roughness Multipliers.
Table 14 - SMACNA Fitting Loss Tables..
Duct Design Sizing Workshec...
Equal Friction Example Worksheet.
Static Regain Example Worksheet.
Quiz I Solutions.
Quiz MI Solutions
‘Work Session I Solution...
‘Work Session II Solution.
REFERENCES:INTRODUCTION
This program covers the fundamental principals
of ir system duct design, primarily for
commercial building applications. The two most
popular duct design methods—equal friction and
static regain—are covered in detail, Although
there are other duct sizing methods used
(velocity reduction, T-method, extended plenum,
constant velocity, etc.) these are not widely used
by designers and are beyond the scope of this
training module. The reader should refer to other
publications for information on these design
methods.
It is recognized that the use of computer-aided
uct design is becoming more and more popular;
however, itis important that the student learn the
manual method of duet design before using a
duct design software program. This will provide
the knowledge necessary to recognize possible
design errors and understand the effects of
various design decisions.
A duct design should only be performed after
the space cooling and heating loads have been
calculated. Once the space loads have been
determined, the air distribution system should be
designed. This includes locating the supply and
return grilles and registers to provide adequate
room ait distribution to the spaces. Load
estimating and room air distribution principles
are covered in other related publications,
After determining the layout (location) of the
supply and return air grilles, the designer must
determine the required sizes of supply and return,
ductwork that will deliver the correct amount of
air to the spaces. Onee the duct sizes and
transition fittings are known, the designer can
determine the total pressure that the fan must
overcome to deliver the required airflow.
Ductwork must be sized properly to ensure that
the air system can be balanced to deliver the
required air volume to each space, An oversized
uot system will be difficult to balance and will
drive up the installed cost of the system, An
undersized duct system will create higher than
necessary air pressure drops, generate unwanted
noise, and will not deliver the required airflow
quantities,
Quizzes and work sessions are included after
each section of this program to assist the student
in evaluating his or her understanding of these
fundamental principles.
DUCT DESIGN CRITERIA
Several factors must be considered when
designing a duct system. Generally, in order of
importance, they are as follows:
* Space availability
«First cost
* Air friction loss
© Room sound level
* Duet heat gain and leakage loss
The sizing criteria will often be defined by the
space available to run the ductwork. Ceiling
plenums, duct chases, and obstructions such as
walls and beams often dictate that a certain size
duct be used, regardless of whether or not it is
the best size from a first cost or air friction loss
perspective.
First cost is often important; however, first cost
mostly impacts the type of materials used to
construct the ductwork, rather than the size of
ducts.
Air friction loss is affected by the duet sizes as
well as the material and fittings used, For
instance, round galvanized sheet metal has the
lowest friction loss per linear foot and flexible
ductwork has the highest friction loss per linear
‘Commercial Duct Designfoot. Also, the quantity of fittings has a direct
effect on the overall air pressure drop of a duct
system, The number of fittings should be
minimized to minimize the duct system
pressure drop and installed cost.
‘An undersized duct system, that is, one with
high velocity, creates noise that is often
‘objectionable to the occupants. Poorly selected
or installed transitions and fittings also create
turbulence, which creates noise and air pressure
drops and should be avoided.
Poorly insulated or large ductwork that runs
through very warm or very cold areas can incur
‘a heat gain or loss that effectively reduces the
capacity of the cooling and heating equipment,
and will likely result in occupant discomfort and
higher operating costs. Leaky ducts have the
same energy-wasting effect, and may create
odors and stained ceiling tiles if duct insulation
becomes wet from the formation of
condensation at the leak points.
CLASSIFICATIONS
OF DUCT SYSTEMS
‘According to SMACNA (Sheet Metal And Air
Conditioning Contractors National Association,
Inc.) standards, duct systems should be classified
with a numerical pressure class as shown in Table
1. ‘These pressure-velocity relationships have
replaced the older terminology, including terms
such as low pressure, high pressure, low velocity,
and high velocity. These older terms are rather
vague and have been replaced with static pressure
classification values.
Note in Table 1 that pressure classes from ¥4" to
3" are designated as either positive (+) or
negative (-) pressure. Pressure classes 4" and
above are for positive pressure systems only.
~~ Static
Premure | resureRangs | Max. Velety
Cin, wag) (in. wg) (ft/min.
tn" O" to 4" 2,000.
a | >and wo | 2.500
| Sia pw | 2.500
or [ aan pw" | 000
ru “>3" and up to 4" 4,000
se [andy =
0 [ >and up o 10 | >
* Determined by designer
‘Table 1 ~ Pressure-Velocity Classifications
Static pressure classifications are much more
usefull than terms such as low velocity because
they may be used fo establish the required duct
construction materials and reinforcing. The
designer and sheet metal contractor may use
these values to establish the required metal
gauge and maximum duet dimensions allowable
to prevent failure, Therefore, for instance, if
someone refers to a SMACNA Pressure Class 4
system, according to the chart, the pressure is
greater than 3.0 in, w.g. and up to 4.0 in. w.g
with a maximum velocity of 4,000 ft/min (fpm).
Over-designing a duet system by using a heavier
than necessary gauge sheet metal will incur
additional cost; therefore the reader should refer
to. SMACNA guidelines for determining
required metal gauges and reinforcing.
DUCT DIMENSIONS
Ductwork is specified and constructed to whole
inch increments, not fractions. Rectangular
ductwork can be constructed to “odd” number
dimensions (7", 9", 11", ete.), but generally most
fabricators prefer to manufacture fittings in even
number dimensions 10 minimize inventory
requirements,
‘Commercial Duet DesignRound duct, especially flexible-type, is readily
available in both even and odd dimensions:
When looking at a set of plans, there are
generally several views available: a plan view,
an elevation view, and a section view. In plan
view, which is the most common duct drawing,
the standard convention for representing duct
dimensions is to always list the first number of
the duct dimension as the visible dimension, In
other words, if a duct is indicated as 36" x 16",
the 36" dimension would be visible and the 16"
dimension would not be shown.
FUNDAMENTALS OF
AIR DUCT DESIGN
Fan and Air Distribution System Components
The primary purpose of an air duct system is to
deliver the proper amount of conditioned air
from the air handler to the conditioned space,
and then to return the air from the space back to
the air handler, as shown in Figure 1.
Supply Fan
——
=r
aL}
Not all air duct systems have both a supply and
return duct, For instance, an exhaust system has
only a return duct, and a hospital operating room
may use all (100%) outside ventilation ait, in
which case there would not be a return air duct
required. In addition, there are circumstances
where it is advantageous to utilize the plenum
space above the ceiling for return airflow. This
is illustrated in the next section,
A typical air system consists of a fan, supply ait
ductwork, transition fittings, discharge grilles,
return air grilles, retum air ductwork, cooling
and heating coil, and filter. The air in the room
is essontially “still air” (15 ~ 50 fpm) and is
typically at atmospheric pressure (zero gauge
pressure).
‘The fan draws air through the retum grille,
return duct, coil, and fan due to the negative
pressure created by the fan, The fan pushes the
air through the supply duct, transition fittings,
and discharge grilles by creating a positive
Pressure at the fan outlet. The total pressure
difference between the inlet pressure of the fan
and the outlet pressure is referred to as the fan
total pressure.
‘The Law of Conservation of Energy
Objects may contain either potential energy or
kinetic energy. Potential energy is derived from
the object’s relative position, that is, its location,
when compared to a reference position, For
instance, an automobile parked at the top of a
hill contains potential energy due to its mass and
the force of gravity, which try to make the car
roll downhill. The brakes produce friction,
which is greater than the force of gravity. If you
release the brakes, the car will roll downhill and
the potential energy will be converted into
Kinetic energy. The word kinetic means motion,
so the faster the car rolls, the more kinetic
energy it has, and the less potential energy it
contains (Figure 2),
A typical fan wheel, driven by an electric motor,
creates pressure and flow because the rotating
blades on the impeller impart kinetic energy to
the air by increasing its velocity, The air leaving
the fan contains air pressure (energy) in two
different forms:
© Static pressure (Sp)
© Velocity pressure (V,)
Commercial Duct DesignPOTENTIAL ENERGY
vs.
KINETIC ENERGY
Potential Energy
(Static Pressure)
Kinetic Energy
(Velocity Pressure)
2
As the high-velocity air exits the fan, the total
pressure consists mostly of velocity pressure
(Figure 3), This velocity pressure begins to
convert into static pressure in the first few feet
of supply air duct, Both velocity pressure and
static pressure exist throughout the entire air
system. Whenever the duct changes cross
sectional flow area, there is a conversion of
yelocity pressure into static pressure.
Velocity Pressure
O jason
Static pressure is a force that is exerted against
the sides of the duct wall equally in all directions
(Figure 4), Static pressure is essentially the
potential energy component in the air.
’
Velocity Pressure
4
An inflated balloon contains all static pressure
If you release an inflated balloon, the static
pressure inside creates a flow of air out of the
balloon, which is actually converting the static
pressure into velocity pressure, The sum of the
static pressure and velocity pressure values is
called the foral pressure and is represented by
the following equation:
ip + Vp
Daniel Bernoulli, a 16th century Swiss
mathematician, physician, and physicist,
developed a concept now known as Bemoulli’s
Law. Bemoulli’s Law simply states that:
whenever there is a change in velocity there is a
corresponding and inverse change in static
pressure. In other words, when velocity
increases, static pressure decreases by the same
amount, causing the total pressure to remain
constant. Likewise, a decrease in velocity causes
an increase in static pressure. This increase in
static pressure is also referred to as static regain
Total pressure, however, always decreases in the
direction of airflow due to friction losses in the
uct, This principle is illustrated in Figure 5.
‘Commercial Duet DesignFor example, let’s assume that the area of duct
section © is 1,0 ft” and that the area of section
Disoon
According to the laws of physics and fluid flow,
the velocity (V) of a substance, in this case air, is
equal to the flow quantity (Q) divided by the
cross-sectional area (4) of the flow conduit, in
‘our case the duict. This can be stated as follows:
For airflow, Q is cubic feet per minute (CFM), V
is velocity (ft/min.), and 4 is ft.
Referring to Figure 5, if we assume that the
airflow rate is 1,000 CFM, we can calculate the
velocity in both sections of duct as follows:
Vie
£000 ft/min / 1.0 f= 1,000 ft/min,
V2 = 1,000 ft/min / 0.6 f= 1,667 ft/min,
Velocity pressure (Vp) for air at standard
conditions (density = 0,075 Ibp/ft') may be
calculated by the following equation:
ry
Pete
7 (
DOs “ A 10000
000 Ree x rN nods
ooo Cen SST XY) 000
‘000 } SAAR soo
3000 5000
= 1000 og
8 000 sooo &
3 a
8 300 100 2
1000 1000
80 700
00 00
400 409
00 300
\80 180
wo |- oo
‘0 0
so +0
0 meee cece it 40
Let it EEN i
op 03 04 0 06 08 al QS 02 03 04 0506 a8 10 15 20 30 40 S060
FRICTION LOSS (IN. WG PER 100 FT OF EQUIVALENT LENGTH)
‘Commercial Duct Design 8However, our friction rate has increased to 0.15
in, w.g./100 ft. E.L. As a designer you will have
to decide if this higher friction rate is acceptable.
For short duct lengths it is probably not a
significant factor, When designing duct systems,
however, it is best to stay as close as possible to
the initial design friction rate, in our ease 0.10
in. w.g/100 ft. E.L.
Velocity Pressure Conversion Line
On the friction loss chart (Figure 9) there is a
line running diagonally from left to right labeled
Velocity Pressure Conversion Line. The velocity
pressure may be obtained by reading vertically
upward from the intersection of the conversion
line and the desired velocity. This line is actually
a plot of the velocity pressure (Vp) equation and
is used to calculate the total friction loss of a
particular section of duct.
Fitting Losses
There are two commonly used methods for
determining the friction losses due to duct
fittings (elbows, transitions, etc.): the equivalent
length method and the total pressure method
The focus of this publication will be on the total
pressure method. The equivalent length method
is discussed briefly; however, you should refer
to other related publications for additional
information,
Equivalent length (E.L.) is a concept used when
referring to components in the duct system other
than straight sections of duct, such as elbows,
‘transitions, and fittings. The component friction
loss is converted into the same (equivalent) loss
as a section of straight duct, For instance, a
rectangular elbow may have an equivalent
length of 18 feet of straight duct. Let’s assume
that the design friction rate for the system is 0.12
in. w.g/100 ft. ELL. By converting the friction
losses of these components into an equivalent
Tength of straight duct, you can add them
directly to the actual length of straight duct to
obtain the total equivalent duct length.
To calculate the total friction loss of the duet
system, including fittings, multiply the friction
rate times the total duct length (f x L) as
ated in Figure 10,
15
12in. wo 00 8
‘Total Length = 18° + 8+ 18°=47
20.121, wa /100" x47 = 0.089 in. wo.
The equivalent length method is widely used for
residential and light commercial applications
However, for larger, more extensive commercial
duct systems, the total pressure method is
recommended,
The total pressure method gets its name from the
fact that you are calculating the total pressure
change across the fitting, As duct sizes change,
throughout the system there is an exchange
between static pressure and velocity pressure.
‘These pressure losses are referred to as dynamic
Josses, and are caused by either a change in flow
direction (as with an elbow) or a change in cross
sectional flow area (as with a transition),
The dynamic loss coefficient, abbreviated C, is a
dimensionless number representing the number
of velocity (pressure) heads lost through the duct
fitting, These values have been determined
through laboratory testing and are published by
ASHRAE and SMACNA. A partial listing of
fitting loss coefficients is included in the
Appendix.
Commercial Duct DesignTo arrive at the total pressure of a fitting loss,
simply multiply the loss coefficient, C, by the
velocity pressure at the fitting as follows:
Tp=Cx¥,
Where:
Tp= Total pressure loss (in. w.g.)
C= Fitting loss coefficient
¥, = Velocity pressure (in. w-g.)
The velocity and corresponding velocity
pressure may be obtained using the equations as
introduced in the previous section.
Example 2~ Fitting Loss Calculation
Note: The Fitting Loss Table is partially
reproduced in the Appendix with the permission
of SMACNA.
Calculate the total pressure loss of the fitting
indicated in Figure 1 (diverging, symmetrical,
rectangular, 90° wye fitting).
wx"
Ayy = 0.69.89
(4, =500 CFM
ZA
x10"
c= 1.3959 fh
0, = 1,000 CF
10x10"
ay = 0.69 54 ft
(yy =500 CFM
“
To calculate the velocity pressure for any fitting
in SMACNA Table 14, pay particular attention
to the notes. For most converging-type fittings,
use the downstream velocity pressure. For most
diverging fittings, you always use the upstream
velocity pressure (see Figure 12 for examples of
converging and diverging fittings).
CONVERGING FLOW DIVERGING FLOW
2
Cross sectional areas and flows are indicated.
The C value is obtained by referring to the
fitting loss coefficient table included in the
‘Appendix under a Type “Y” fitting (Table 14-
14). For a @ = 90° wye fitting, the loss
coefficient is read as 1,0,
Since the flow through each branch is the same,
the pressure losses are also identical. First, solve
for the velocity:
V=QIA;
1» = Von = 500/0,69 = 725 fpm
and
Ve = 1,000/1.39 = 719.4 fpm
Now solve for the velocity pressure:
Vpo= (We/4,005) = (719.4/4,005)° = 0.032 in, w.2.
Finally, we solve for the fitting total pressure
loss:
Tp=Cx Ve=1.0 x 0.032 =0,032 in, w.g.
‘Commercial Duet DesignFriction Losses in Straight Duct
Duct friction loss is affected by the following:
* Airvelocity
@ Duct size and shape
* Duct material roughness factor
© Duct length
ing any one of these variables will affect
the air friction loss. Other synonymous terms are
often used when referring to friction loss in air
systems such as “air pressure drop”, “static
* and “coil pressure drop”. In most
cases these terms are all used with reference to
units of inches of water gauge (in. w.g.).
Duct material roughness refers to the inside
surface of the duct material, The rougher the
surface, the higher the friction loss. Most duct,
sizing tables use the roughness factor for
smooth, galvanized sheet metal as the reference
value, For other duct construction materials such
as duct board, flexible duct or duct liner, a
multiplier is used to correct for the higher value.
A duct roughness multiplier table is included in
the Appendix.
Example 3 ~ Material Roughness Correction
What is the correction factor for converting from
smooth, galvanized sheet metal to rigid
fiberglass duct board for a supply air system?
Using the Duct Roughness Multiplier Table 4 in
the Appendix, the correction factor is read as
1.32, In other words the friction rate for rigid
duct board is 32% higher than smooth sheet
metal duct per given length. This correction
factor is multiplied by the design friction rate
prior to selecting the required round duct size.
For instance, in the previous Example | for the
18 in, duct, the friction rate was 0.10 in,
w.g/100' E.L. For rigid duet board the design
friction rate is 0.132 in, w.g./100 fl. E.L, (1.32 x
0.10),
If you desire (0 use a design friction rate of 0.10
in. w.g/100 ft. E.L., and you are using rigid duct
board, then you must determine the required
friction rate for the smooth, round duct that is
equivalent to a friction loss of 0.10 in. w.¢/100"
E.L. To arrive at this value, simply divide the
desired friction rate by the correction factor as
follows:
(0.10 in. w.g./100 ft. B.L,) / (1.32) = 0.076
in. w.g./100 ft. ELL.
Now you use this new friction rate for sizing all
duct sections that are to be made from rigid duct
board. In effect, you are increasing the size of
the duct to account for the higher friction loss
per unit length,
Round vs. Rectangular Duct
of Equal Friction Rate
Ata given velocity, round duets have the lowest
static pressure drop per linear foot of any duct
shape. Figure 13 indicates the relationship
between duct shape and frietion loss,
Notice the ratio of perimeter to area is the lowest
for a round duct, Less duct surface area
translates into less air ftiction loss. As you
increase the aspect ratio (longest dimension
divided by the shortest dimension) the ratio of
perimeter to area increases proportionally. The
last example illustrates a duct with an aspect
ratio of 9:1. This is a highly undesirable shape
for an air duct, as the friction loss is nearly twice
that of a square duct of the same cross-sectional
area. In addition, ducts with large aspect ratios
have more heat gain than smaller aspect ratio
duets.
ul
Commercial Duct Designfata Fin
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toArea | Round Duct | 15,090 cr
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43
Large aspect ratio ducts are more difficult to
reinforce structurally and may exhibit what is
commonly referred to as “tin canning”. Tin
canning occurs when the fan tums on and off and
the duet walls actually flex in and out due to the
air pressure changes inside the duct, causing a
loud, disturbing, thumping sound. Since it
hhappens each time the fan tus on or off, you can
imagine what the occupant’s reaction will be
As a general rule of thumb, duct aspect ratios
should be limited to no more than 4:1.
Round ducts are often used for branch duets off
rectangular main ducts. Round duet unfortunately
requires a larger height clearance when compared
to rectangular duet. This is illustrated in Figure 13,
with a 3 ft. x 3 fl. square duct having a cross
sectional area of 9.0 fi’, The equivalent round
duct diameter for the same area is 39.4 in, This
means that an additional 3.4 in, of height is
required when using a round duct for this
particular example. Saving space is one reason
many designers use rectangular trunk ducts
Round Duets of Equal Velocity
and Equal Area
Duct systems are generally sized first as round
ducts, Then they are converted to rectangular
sizes of equivalent friction rate, Most friction
charts are constructed for round duct (see the
friction loss chart in the Appendix). You cannot
simply calculate the area of the circle (round
uct), then use a rectangular duct with the same
cross-sectional area. Doing so would create a
duct with a higher pressure drop than the round
duct of the same area. This goes back to the ratio
of perimeter to area shown in Figure 13. The
velocity in a rectangular duct with equivalent
friction rate will be less than the velocity in the
round duct, This is necessary so that the pressure
losses for the two ducts are equal
To accomplish this conversion from round duct
to an equivalent rectangular duct, refer to Table
1 in the Appendix.
Commercial Duct Design
2Example 4 — Converting From Round to
Equivalem Rectangular Ducts
Convert a 22 in. round duct to an equivalent
rectangular duct with a maximum aspect ratio of
3:1.
In Table 1 of the Appendix you will find the
rectangular duct dimensions listed along the top
and left side scales,
Now the trick is to find a combination of
dimensions that meet the criteria stated above;
that is, a maximum aspect ratio of 3:1 and a 22
in, round duct. Refer to Figure 14. Note there are
‘two numbers under each column, area (sq. ft.)
and diameter (in.). Scanning down the first
column (6 in. side) you are looking for a
diameter of 22 in. I's not under the first column,
as the largest diameter is a 16.5 in. duct. Now
look under the 8 in. column, There is a 22 in,
diameter duct listed for the 64 in, side duct.
However, the 8:1 aspect ratio (64/8) violates the
3:1 aspect ratio limit, Continue over to the 10 in.
column, Read down till you see the 21,9 in,
diameter, This equates to a 46 in, duct, which
makes our aspect ratio 4.6:1, still oo large. Read
over to the 12 in, column, then read down to the
21.9 in, diameter corresponding to a 36 in. duct.
‘That works, as the aspect ratio is 3:1 (36/12).
There are other combinations of values that also
work, such as 14" x 30", 16" x 26", 18" x 24"
and 20" x 20",
Designers generally attempt to use the larger
dimension for the width and the smaller dimension
for the height. This is due to the fact that available
space to run duct above most ceilings is usually in
short supply. Also, try to maintain one of the duct
dimensions (either height or width) whenever
possible when transitioning fiom one duct size to
the next, This saves money during fabrication by
simplifying the transition,
Other Pressure Losses
There are additional factors that affect duct
system pressure losses that relate to the physical
characteristics of the fan inlet and outlet
conditions.
Fan Outlet Static Pressure Loss or Gain
Fan outlet static pressure loss or gain must be
included in determining the required fan static
pressure, The SMACNA fitting loss. tables
included in the Appendix contain loss
coefficients that account for various orientations,
such as converging or diverging flow at the fan
discharge.
‘Commercial Duet DesignOF RECTANGULAR DUCTS FOR EQUAL FRICTION.
CIRCULAR EQUIVALENT DIAMETER,* EQUIVALENT AREA AND DUCT CLASS}
Commercial Duct DesignSystem Effect
A fan/duct system with an improper fan outlet ot
inlet connection will result in a reduced airflow
quantity, less than the manufacturer's published
ratings. Fans are generally rated, designed and
tested with open inlets and with a section of
straight duct connected to the outlet of the fan,
In reality most installations do not have open
inlets or adequate lengths of straight duct
attached 10 the fin outlet. This condition is
commonly referred to as system effect (see
Figure 15), System effect is a de-rating factor
used to predict the reduction in actual fan
performance caused by these physical
limitations placed on the fan system. When there
is less than 100% effective length of straight
duct directly off the fan outlet, like an abrupt
transition or elbow, system effect should be
considered,
The effective duct length depends on the
particular characteristics of the fan design, but in
general is a length of duct whereby the velocity
of the air flowing inside the duct reaches a
uniform velocity profile, This is generally
defined as a length of 2-1/2 duct diameters for
ducts with velocities of 2,500 fpm or less.
LAST AREA,
PiscHance:
Buet
\
}
Se
FAN HOUSING
er
15%
CENTRIFUGAL.
100% EFFECTIVE DUCT LENGTH
TO CALCULATE 100% EFFECTIVE DUGT LENGTH, AS-
SUME A MINIMUM OF 2 DUCT DIAMETERS FOR 2600
FPM Of LESS.ADD 1 OUCT DIAMETER FOR EACH AGDL
TIONAL. 1000 FPM,
EXAMPLE: 5000 FPM = 5 EQUIVALENT DUCT DIAMETERS.
IF DUCT IS RECTANGULAR WITH SIDE CIMENSIONS a
AND b, THE EQUIVALENT DUCT DIAMETER IS EQUAL TO
Commercial Duet Design‘A considerable amount of subjective judgment
must be applied when working with system
effect factors, as there may be a wide variation
in different manufacturer’s fan designs. It is
important to check for system effect in the total
pressure analysis of the fun, The reader should
refer to ASHRAE and SMACNA publications
for additional information on system effect
Wind and Stack Effects
The effects of wind blowing directly into
building air intakes or exhausts should be
considered, Intakes and exhausts should always
be located away from prevailing winds.
Infiltration also has a negative effect by
imposing an additional load on the cooling or
heating system since unconditioned outside air is,
introduced directly into the spaces.
In tall buildings or in instances where the outside
temperature is colder than the inside temperature,
air tends (o move from the lower areas to the
higher areas. Natural paths are via elevator shafts,
equipment chases, and stairwells. This movement,
of air ig referred to as normal stack effect. During
the summer, or when the outside temperature is
‘warmer than the inside temperature, the opposite
effect can occur, referred to as reverse stack
effect. Since cool air is heavier than warm air, the
building air tends to drop. You may have
experienced this phenomenon when exiting an
elevator of a tall building.
SMACNA and ASHRAE publications list
various formulae and have examples of how to
calculate stack effect. It is mentioned here only
to bring it to the reader's attention.
This concludes the introduction and the
fundamentals of airflow through ducts. It is
recommended that you complete Quiz. I located
at the back of this book in order to test your
understanding of these important concepts.
Commercial Duct DesignSTEPS REQUIRED TO DESIGN AN AIR DUCT SYSTEM
Before we begin sizing ductwork, a few
preliminary tasks are required, Figure 16
indicates the steps required to design an air duct
system.
AIR SYSTEM DESIGN STEPS
@ Dotormine Number of Zones
@® Perform Cooling & Heating Load Estimate
@ Detrmine Rone Aiflow Guanes (CF)
@® Select Duct Materia! (Sheet Metal, Fiborglass, Flex)
© Loca Gils & Reis and Lay Out Ductwork
® Summarize Duet Airflow Quantities (CFM)
® Size Ductwork From Fan Out to Extremities:
@® Calculate Air System Pressure Lossas
@® Selact and Adjust Fan
Step 1: Zone Selection
Determine the number of unique temperature
control zones that will be required. Perimeter
and core areas should be separated into zones
depending on variations in internal loads and
building exposure (N, 8, E, or W). Further sub-
zoning into additional control zones may be
accomplished if necessary. Executive offices,
conference rooms and computer rooms are all
examples of sub-zoning that may be
accomplished.
Step 2: Cooling and Heating Load Estimate
‘The importance of an accurate cooling and
heating load estimate cannot be over-
emphasized. Computer software programs are
readily available, inexpensive, easy-to-use, and
represent the best method of performing an
accurate cooling and heating load estimate. A
computer-calculated load estimate projects a
professional image of your company to your
customers or clients. Whether it’s fact or fiction,
@ computer printout is usually accepted at face
value and lets the customer know that you take
the extra steps necessary up-front to ensure that
the job is done accurately and correctly. OF
course, a computer program does not replace
years of experience and should only be
lered another tool in your toolbox.
‘An inaccurate load estimate results in oversized
or undersized equipment, leading to an
inadequate, poorly performing system and likely
an unhappy customer.
Step 3: Determine Room/Zone Airflow
Quantities
The results of a load estimate calculation include
the airflow quantities required for conditioning
each of the rooms or zones, The sum of these
Zone airflow quantities is the total amount of air
the fan must deliver, also referred to as the total
supply air quantity. This value is used to size
both the fan and the first section of supply duct
off the fan,
‘The subject of load estimating includes a
concept known as the block load. The block load
is simply defined as the maximum cooling load
for the entire building that occurs throughout the
year. For most residential and light commercial
buildings located in the Northen Hemisphere,
this maximum load occurs late in the afternoon
during the hottest summer month, typically 4:00
PM in July or August. In addition, computer
programs generally calculate a room-by-room
cooling load and coincident room airflow
quantity. These room-by-room airflow quantities
are used to size the zone supply diffusers and
return grilles, as well as the branch ducts that
serve them. The sum of these airflow quantities
is used to calculate the main duct section sizes.
Commercial Duet DesignLoud estimating and room air distribution
principles are covered in greater detail in other
related publications, The scope of this program
will be limited to the task of duct sizing.
Step 4: Select Duct Construction Materials
After calculating the cooling and heating loads,
the designer decides which materials and shape
of duct to use. Common duct construction
materials used in residential and light
commercial applications include:
# Fiberglass duct board
© Galvanized sheet metal with either internal
lining (Liner) or external insulation (wrap)
© Flexible vinyl-coated with helical wire core
Most commercial applications use galvanized
sheet metal for the main duets and either flexible
duct or sheet metal for the branch ducts. Flat
oval spiral ductwork is used on high-pressure
systems and will not be covered in this text.
There is generally a trade-off between duct
material and price. Fiberglass duct board is
relatively inexpensive and easy to install;
however, the pressure loss is approximately 30%
higher than that of smooth galvanized sheet
metal, Flexible (flex) duct is easy to install but
exhibits a much greater (three times higher)
pressure loss per linear foot as compared to
smooth sheet metal, And that is when the flex
duct is hung straight, If flexible duct is allowed
to unnecessarily sag and bend, the pressure loss
will be much greater. Poorly installed flexible
duct is one of the most commonly encountered
field problems and should be avoided.
Duct insulation may be internal (also referred to
as duct lining) or external (also referred to as
duct wrap). Rectangular duct dimensions are
expressed in outside dimensions, regardless of
whether there is an intemal lining. Round duct
dimensions are always assumed to be inside
diameter (LD.). Internal fining is sometimes
used in the first section of duct after the fan to
attenuate noise generated by the fan,
As mentioned before, internal lining has a higher
pressure loss than smooth sheet metal and has
been the subject of some academic discussion
relating to indoor air quality (IAQ). Some in the
scientific community claim that the porous
nature of fiberglass duct liner creates an
environment to harbor and incubate the growth
of mold spores and other microorganisms.
However, this is not generally a problem,
provided adequate air filters are used {0 prevent
the accumulation of dust and dirt on the internal
duet wall surfaces.
Some designers choose to externally insulate
(wrap) duct surfaces instead of lining the
interior, This prevents the fiberglass from
coming into contact with the supply air stream
and to facilitate cleaning of the duct wall
surfaces. The designer should be aware that
unlined ductwork has the potential to be noisier,
and proper acoustic design measures should be
taken to prevent this from occurring,
One final comment about duct insulation;
remember {0 allow extra room for the duct liner
or insulation, Duets with a 1” intemal liner must
be sized 2" larger on each dimension (height and
width) to account for the liner. In other words, a
10" x 12" duet with internal liner must be
fabricated 12" x 14" to accommodate the liner.
Likewise, when using externally-wrapped duct
be sure to allow for the extra height or width
required.
Step 5: Locate Gi
Out Duct System
Jes and Registers and Lay
Laying out the duct is simply producing a sketch
of where to route the duet from the fan to each
of the zones, As the old saying goes, a straight
line is the shortest distance between two points.
Therefore, unnecessary tums and bends should
be avoided. As a general rule, every elbow adds,
the same air pressure drop as 15-20 feet of
Commercial Duct Design
18straight duct. Try to allow at least a few feet of
straight duct directly downstream of the fan
before you make any turns or take-offs, The air
in the duct is very turbulent in the first few feet
of duct downstream of the fan. The air needs a
few feet of straight duct to establish a uniform
velocity profile so that all of the energy from the
fan can be converted into pressure, Any energy
not converted into pressure becomes turbulence
and vibration, which will likely lead to a noisy
system and customer complaints,
As mentioned in the previous section, system
effect will occur if a uniform velocity profile is
not produced prior to an elbow, If it is necessary
to have an elbow close to the fan, always turn
the air in the same rotation direction as the fan
Draw a preliminary single-line schematic of the
duct system from the air handler(s) to each of
the zones by the most efficient and economical
route, avoiding unnecessary tums and bends. A
semi-transparent paper such as “onion skin” or
“velum” should be used to sketch the duct
system over the architectural floor plan, Be sure
to refer to reflected ceiling plans and structural
drawings to avoid interference with plumbing,
sprinklers, lighting, and structural beams.
Label the duct sketch with numbers and/or
letters identifying every point on the duct system.
where there is either a change in flow quantity or
a change in direction. This includes all transition
fittings, elbows, branch take-offs and the
connection to the air handler,
Transfer these duct section labels to an
appropriate worksheet (refer to the Duct Design
Sizing Worksheet in the Appendis).
Select supply outlets in each zone based on the
zone airflow quantities calculated in the load
estimate performed previously. Supply outlets
should be selected based on their published and
rated airflow quantity, pressure drop, and throw.
‘To minimize heat gain and loss, duets should not
be located in extreme temperature areas such as
hot attics whenever possible. If you must route
duct through extreme temperature environments,
be sure to use adequate insulation to minimize
thermal losses.
Don’t forget the return air duct system design.
Return air grilles may be located in each zone or
alternatively located in a central area such as a
hallway or corridor. If you are locating the
return air grille in a central area, be suze that the
supply ait is able to escape areas with closed
doors. Undercutting of doors or the use of
transfer grilles may be necessary. A tightly
sealed room will not receive adequate supply air.
Some buildings with multiple floors use a
ceiling plenum return for the return air, therefore
a ducted return air system may not be required
Generally, ceiling plenum retums are used only
on intermediate floors of a multiple story
building and not in top floor attic areas due to
the heat gain from the roof (Figure 17).
19 Commercial Duet DesignFoot Heat
Sa 7
vm %@ te
Cling Plenum Return
Ducted Retuin Air
Supply and return outlets should be located to
provide adequate room air distribution to the
zones, Room air distribution is covered in
another related publication.
Step 6: Summarize Duct Airflow Quantities
(CFMs)
As discussed previously in Step 2, the zone-by-
zone load calculation will yield the required
airflow quantities, Beginning at each zone,
working against the direction of airflow back
toward the fan, sum the airflow quantities from
each outlet to the branch duct sections then
finally back to the main trunk duct, finishing at
the fan outlet, This total airflow quantity should
equal the amount calculated by the load
estimate
Finally we get to the fim part. The next task is to
determine the required sizes of supply and return
ductwork that will deliver the correct amount of
air to the spaces, Beginning with the first section
of duct off the fan, this section is sized based on
an assumed initial velocity. Subsequent duct
sections should be sized by the appropriate
sizing method, from the fan out to the most
distant points, The equal friction and static
regain methods of duct design are illustrated in
the following sections.
Do not over-design the duct system by
systematically downsizing each trunk duct
section after each branch take-off. Often it is
more cost effective to maintain a constant duct
size for several branch runs. Duct transitions are
expensive to fabricate and costly to install.
Once the duet sizes and transition fittings are
known, the designer can then determine the total
pressure that the fan must overcome to deliver
the required airflow. Transition fitting losses are
covered later in a separate section of this
manual.
You should always use a Duct Design Sizing
Worksheet, like the one found in the Appen
to organize your calculations.
Step 8: Caleulate Air System Pressure Losses
Once the duct sections have been sized, you may
summarize the air pressure losses from both the
supply and return duct systems. This is often
referred to as the external static pressure
because these losses are “external” to the air
conditioning unit. Manufacturers generally
publish fan ratings and fan curves based on
extemal static pressure; that is, internal losses
due to coils, filters, ete. are accounted for in the
cataloged fan ratings.
‘Commercial Duct DesignDetermine if calculated duet sizes will fit into
the allowable space. If not, adjust sizes or aspect
ratios to fit. Do not forget to allow space for
either intemal duct Jiner or external duct
insulation,
Step 9: Select and Adjust Fan
In Step 8 we summarized the static pressure
losses for the duct system. To this amount we
add any pressure losses due to filters, dampers
and any other components in the duct system to
arrive at a value referred to as the total static
pressure. This total amount is the pressure that
the fan must overcome to deliver the required
amount of ait. This total amount is also used to
select the required fan motor size.
Once the fan is selected and installed, an air
balance should be done. This involves
measuring the fan speed (rpm) and total pressure
drop across the fan as well as measuring and
summarizing, the airflow at all of the diffusers.
These measured values should be compared
against the required values from the cooling and
heating load estimate, Balancing dampers are
adjusted to attempt to deliver the correct amount
of air to cach zone. Often the actual airflow
being delivered is less than or greater than
required and the fun pulley (sheave) may require
adjustment or resizing,
DUCT SIZING METHODS
The two most common methods of sizing
subsequent duct sections in use today are:
© Equal friction
© Static regain
While other duet sizing methods exist (such as
the T-method, velocity reduction, total pressure,
and constant velocity methods), they are not
widely used and are not included in this text
Readers interested in learning more about these
other methods should consult ASHRAE,
SMACNA, ACCA, or other related publications,
With the equal friction method, as the name
implies, ducts are sized for an equal (constant)
friction loss per unit length. In its purest form,
this uniform friction loss per linear foot of duct
is held constant for the entire duct system. The
equal friction method is the most widely used
method for sizing lower pressure systems. This
method automatically reduces the velocity of the
air in the direction of flow. Therefore some
“regain” of static pressure is created, however it
occurs in unknown amounts and is not usually
accounted for.
Once initial sizes are calculated, the total
pressure of all sections should be calculated and
noted. Sections should then be resized to
equalize the pressure at all junctions, This is
demonstrated later in the example problem.
‘The equal friction method is generally used
when sizing retum and exhaust systems,
The primary disadvantages of the equal friction
method are:
There is difficulty in balancing branch flow
rates, even with balancing dampers
2. It cannot ensure a uniform, constant inlet
pressure to variable air volume devices and
terminals.
To overcome these disadvantages, modifications
to the equal friction procedure have been made.
This is sometimes referred to as the modified
equal friction design procedure. This procedure
is used whenever the duct system is non-
symmetrical or for systems with both long and
short duct runs. ‘The modified equal friction
design procedure is described in detail later.
The static regain method of duct sizing is a more
complex and sophisticated method and may be
used to size supply duct systems of any pressure
21
Commercial Duct Designor velocity, The advantages often outweigh the
extra. work involved in performing the
calculations, In this method, the velocities are
systematically reduced, resulting in a conversion
of the velocity pressure into static pressure, which
‘overcomes a portion of the ai tion loss in the
next downstream section of duct.
This phenomenon is not totally efficient,
however. A regain efficiency of 75% is assumed
for most average duet systems. This method is
also advantageous because it creates a self
balancing system, in that all gains and losses are
proportional to the velocities. This makes it
especially usefull for higher-velocity systems,
where the turbulence and noise generated by air
balancing dampers prohibits theit use.
The main disadvantage of the static regain
method is the larger duct sizes that result. This
translates into higher first cost; however, the
reduced static pressure on the fan often results in
a lower fan operating cost over the life of the
system
Note: The SMACNA fitting loss coefficient
tables included in the Appendix account for all
static regains or losses that may occur. You
should not add additional regain or losses 10 the
system due to fittings or trans
ms.
EQUAL FRICTION DUCT
DESIGN PROCEDURE
This method assumes that the user has already
completed the required steps as outlined in the
previous “STEPS REQUIRED TO DESIGN AN
AIR DUCT SYSTEM” section. Refer to Figure
18 for illustration
ro
40" x 20’ Fan Outlet
Supply Grille Loss = 0.10 in. wg.
18
The following design procedure is recommended
‘when using the equal friction method:
The first section of duct downstream of the fan
is not sized by any particular method (equal
friction or static regain). Rather, it is sized based
on an assumed initial velocity. Designers
sometimes size the first section of duct to be the
same size as the fan outlet connection, provided
the outlet velocity is within an acceptable range.
Remember to try to provide several feet of
straight duct directly off the fan to prevent
system effect from occurring. Recommended and
maximum velocities are listed in Table 2 of the
Appendix.
Remember that the friction loss values that
appear on the friction chart are for round,
galvanized, smooth sheet metal duet. If you are
using a duct material other than galvanized sheet
‘metal, you will need to correct the friction factor
indicated. This is done by applying a material
correction factor, which is listed in the
Appendix. If you are not using round duct you
must first size the system as round duct then
convert the round sizes to equivalent rectangular
dimensions by using the conversion table (Table
1) included in the Appendix
Commercial Duct DesignThe use of flex duet should be minimized and
used in no greater than 8-10 lengths since the
equivalent pressure drop of flex duct is over
three times that of galvanized sheet metal,
In the example duct system shown in Figure 18,
we have a 40" x 20" fan connection, Since most
fan outlets are rectangular in shape, you will
generally have to supply a transition from the fan
outlet dimensions to the dimensions of the first
duct section. Let’s assume that we will be using
rectangular, smooth shect metal duct for this
system. From Table 2 in the Appendix, for a
general office we will use a maximum velocity
of 1,500 fpm, which is the controlling factor for
noise generation. The total airflow in section @ is
7,500 CEM (2,500 3).
Since we now know the velocity and airflow we
can solve for the area:
A= O/V=7,500 CFM / 1,500 fpm = 5.0 f?
Now enter Table I (Circular Equivalent Diameter)
in the Appendix and locate a combination of duet
dimensions with an area equal to or greater than
5.0 £°, From Table | we find that there are many
possible combinations of duct dimensions with an
area of 5.0 £, Since the fan outlet is 40" x 20",
let’s check the velocity using the same size duct as
the fan outlet. From Table I for a 40" x 20" duct,
the equivalent area is 5.07 ’, which is adequate,
Therefore, a transition from the fan to duct seetion
@ is not required and there is no fan outlet gain or
loss to consider. In Table 1, under each column of
duct dimensions, there is a value labeled “Diam,
in.”. This is the diameter for a round duct with an
equivalent friction loss. For a 40" x 20"
rectangular duct, the round equivalent is 30,5".
Next, on the friction Joss chart, locate the 7,500
CEM fine on the vertical axis. Follow this line to
the right until it intersects with the 30." round
duct line. Now read vertically to determine the
friction loss value, in our ease 0,085 in. w.g/100
ft. E.L. This means that for a flow rate of 7,500
CFM, for a 30.5" round duet, the friction loss for a
100 fl. length section will be 0.085 in, w.g. But
section ® is only 40 fi. long. The corresponding
friction loss for section ® will therefore be: 0.085
x (40/100) ~ 0.034 in, w.g. This corresponds to a
velocity of approximately 1,500 fpm, which may
be read from the friction chart. We will use this
friction rate (0.085) to size the remaining duct
sections,
Using the Duct Design Sizing Worksheet
included in the Appendix, enter the information
‘we know thus far
The next element in the system is the outlet in
section ® with an airflow rate of 2,500 CFM.
The outlet loss is given as 0.10 in. wg. You
should consult actual grille and register catalogs
when designing duct systems to determine the
appropriate friction losses. Add this known loss
value to the worksheet.
Next we come to duet run C-D. Since the
airflow quantity is reduced significantly (7,500 —
2,500 = 5,000 CFM) we need to transition to a
smaller duct. To determine the required
rectangular dimensions of section @ we must
first find the required round size then convert it
to a rectangular equivalent. Refer to the Frietion
Loss Chart and use an equal friction rate of
0.085 in, w.g/100 ft. E.L., Determine the
intersection of the airllow quantity (5,000 CFM)
with the friction rate. The intersection point falls
very close to the 26” diameter line, Now refer to
Table 1 and locate a combination of rectangular
dimensions that are close to a 26" diameter.
‘There are several possibilities. As mentioned
previously, it is generally a good idea to try to
maintain at least one of the dimensions when
transitioning duet sizes. This makes the fitting
less difficult to fabricate and saves money too.
Let’s maintain a constant duct height of 20" and
vary the duct width. From Table 1 we will select
a 28" x 20" size for section ®, This size is
equivalent to a 25.7 round duet with a velocity
of approximately 1,400 fpm and a friction rate of
0.095 in, w.g./100 f. ELL.
2
Commercial Duct DesignBefore we continue we must calculate the
friction loss due to the transition between
sections @ and @, Refer to the SMACNA
friction loss tables, specifically Table 14-12,
Fitting Type A, which is a converging
rectangular to rectangular fitting, To determine
the fitting loss coefficient, C, we must know the
ratio of areas between the two duct sections
along with the transition angle, @, Let’s assume
that the transition angle is between {5-40°. The
ratio of areas (A;/A) = (5.07/3.60) = 1.4, From
the table for Fitting A, the corresponding loss
coefficient is 0.05 (smallest value in table). To
calculate the total loss we use equations 3 and 4
as follows:
Vp= (V/4005)? = (1,520/4005) = 0.144 in. w.g,
Tp =Cx Vp=0.08 x 0.144 = 0.007 in, w.g.
For all practical purposes, this is an insignificant
amount. Altematively, we could have read the
velocity pressure direetly from the Friction Loss
Chart or the Velocity Pressure Table (Table 3),
You should note that the total pressure loss due
to a fitting is much more influenced by the
velocity rather than the fitting loss coefficient,
C. Had the velocity in the previous example
been say twice as high, the pressure loss would
have increased by a factor of four times due to
the “squared” relationship between pressure and
velocity, Add these values to the worksheet.
The last element in duct run C-D is the outlet,
with a flow rate of 2,500 CFM. Again, this loss
is given as 0.10 in. w.g. Add this value to the
‘worksheet.
The final duct run is D-E. Similar to the
previous section we have another transition
since the airflow is reduced to 2,500 CFM. We
will maintain our previous duct height of 20"
and locate the width required. As before, we
must determine the required round duct size and
then convert it to an equivalent rectangular size.
From the Friction Loss Chart find the round duct
size corresponding to the friction rate of 0.09 in.
w.g/100 ft. E.L, A 20" round duct meets our
requirements for section ®@. Next, in Table 1
locate a round duet with a 20" diameter that
corresponds to a duct height of 20", A 20" x 16"
duct has an equivalent diameter of 19.5 in., a
round duct velocity of 1,200 fpm, and a
corresponding friction rate of 0.10 in. w.g/100
fi. E.L. Add these values to the worksheet.
Now we may calculate the loss due to the
transition between sections ® and @. This
transition is the same as the one before. Since
we now know the sizes of both sections, we may
once again calculate the ratio of areas as
follows: (AVA) = (3.60/2.07) = 1.7. The loss
coefficient, C, is the same as our previous
calculation, 0.05.
‘We are now ready to calculate the total friction
loss of each duct run. From the Duct Design
Worksheet we see that the total section loss for
duct run A-C is 0.134 in, w.g. For duct run C-D
the total friction loss is also 0.136 in. w.g. Duct
run D-E also has a section loss of 0,136 in. w.g.
The next step is to determine the duct run with
the highest friction loss starting at the fan and
proceeding all the way to the furthest duct ran,
or the run with the most fittings. On large
systems this is somewhat of a tedious task;
however, for our simple system it is easy to see
that duct rin A-E is the run with the highest
friction loss.
Summarize the total friction loss by adding the
individual section losses beginning at the fan
and ending at the outlet in section C-D, This.
calculates to be 0.206 in. w.g. We will round this
value to 0.21 in. w.g
Comparing the section friction losses, they are
within 0.05 in, w.g. of each other. Therefore air
balancing will be easy to accomplish by the use
of balancing dampers.
Commercial Duet Design
24Remember to allow room for either internal duct,
lining or external duct wrap (insulation) when
designing duct systems. For example, if duct is
wrapped with I" insulation and you only have
12" of clearance to run a duct, the largest duct
height you can use is a 10" duct. Likewise, a 12"
duct with a 1" lining is actually only a 10" duct
when it comes to calculating flow area
This completes our calculations for the equal
friction method,
MODIFIED EQUAL FRICTION
DUCT DESIGN PROCEDURE
This method was created to allow for easier air
balancing of duct systems that have non-
symmetrical layouts; i.e., some short duct runs
along with some longer runs. The idea is that
you size the main trunk duct using the equal
friction method, then slightly downsize the
branch runs that have low pressure drops. This
minimizes the tequirement to “choke” off the
airflow (in the shorter duct runs) with manual
balancing dampers.
The equal friction method, by definition, means
that the friction loss per linear foot remains
relatively constant for all duct sections, Using this
method causes the shorter duct runs, as well as
those closer to the fan, to receive more air than
they are supposed to receive (because the total
pressure drop in those sections is lower) and
‘causes the longer duct runs to receive less air, The
designer will often place manual balancing
dampers in each duct run to intentionally restrict
the airflow in those sections and create an
additional pressure loss such that the total pressure
loss for the shorter duct sections will equal the
pressure loss on the longer duct sections.
With the modified equal friction method, the goal
is to slightly downsize the branch runs closer to
the fan or those sections with lower pressure
drops. This has the same effect as closing a
balancing damper and choking the flow.
The advantage of this method is twofold: first,
the use of smaller ducts saves money, and
secondly the smaller ducts allow for easier
balancing of the air flows. Keep in mind,
however, that downsizing ducts creates higher
velocities. You should not downsize to a point
where it violates the recommended velocity
range values. High velocities may create
unwanted noise.
Finally, if you do downsize duets slightly in the
shorter runs you should still utilize balancing
dampers at cach branch take-off to assist in air
system balancing. The most precise duet design
may theoretically work on paper and may not
get installed exactly as designed. It may need
some “tweaking” after start-up.
Both the equal friction method and the modified
equal friction method of duct sizing are
demonstrated in the work session.
STATIC REGAIN DUCT
DESIGN PROCEDURE
The static regain method of duet design is more
complex and time-consuming that the equal
friction method. Often a trial-and-error
procedure is necessary. Therefore the use of a
‘computer program is highly recommended for
designing large duct systems using the static
regain method.
When designing a duct system by the static
regain method, the objective is to size the
subsequent downstream duet sections by
systematically reducing the velocity (and
corresponding velocity pressure), which creates
an increase in static pressure that offsets the
friction Joss in the next duct section. As
mentioned previously this conversion of velocity
pressure to statie pressure is not completely
efficient. Regain efficiencies range from 75% to
90% under ideal conditions, However, most
designers use 75% as the average regain
efficiency.
25
Commercial Duct DesignTo reiterate, the primary advantage of this
‘method of duct design is the fact that the system
‘will tend to stay in balance much better because
the pressure changes in each section are directly
proportional to the velocity changes. This makes,
it especially useful for designing variable air
volume (VAV) systems. The disadvantage is the
fact that the ducts tend to be larger on the end
sections, which adds to the installed cost,
Let’s redesign the simple duet system shown in
Figure 18 using the static regain procedure.
Once again, the objective is 10 oversize the
downstream duct sections to create a regain of
static pressure that will help offset the friction
losses in the next section.
First, section ® will remain the same size as
before, 40" x 20", but we will increase the sizes
of sections @ and @ to reduce the velocity
pressure and increase the available static
pressure in those sections, Section @ was
previously a 28" x 20" duct, Let’s increase the
size to a 30" x 20" duct. From Table 1 we
determine the equivalent round diameter is 26.7
in, From the Friction Loss Chart we read the
friction rate as 0.08 in, w.g/100 ft. E.L. and the
velocity as 1,320 fm. Add these values to the
worksheet,
Next we proceed to section ®. Previously it was
sized as a 16" x 20" duct so let's upsize to an
18" x 20" duct. From Table 1 we read an
effective round diameter of 20.7 in. From the
Friction Loss Chart we read the friction rate as
0.075 in. w.g./100 fi. E.L. and a velocity of
1,070 fpm. Enter these values on the worksheet.
Next we need fo account for the transition fitting,
between sections ® and ®. The ratio of areas
(AWA) is (3.89/2.34) = 1.6; therefore, the
C-value is 0.05 as before.
‘The final element in the duct system is the outlet
at the end of section ®. Add the information to
the worksheet,
‘We are now ready to sum the pressure losses as
we did before. The results indicate a total
extemal static pressure of 0.19 in, wg,
approximately 10% less than the equal friction
‘method, which was 0.21 in, wg
To reiterate, the larger duct sections will be
more expensive to fabricate and install, Also,
lower velocities mean slightly higher duct heat
guins, although in our simple example it would
‘de negligible. On large systems, you will have to
calculate the fan energy savings and compare
that to the higher initial installed cost. Since
‘most duct systems last at least 20 years and fans
consume approximately 30% of the total
building energy, on average, there may be a
sound economic argument to be made for using
the static regain duet design method.
SMACNA and ASHRAE have developed the
fitting loss coefficient tables included in the
‘Appendix, It is very important to understand that
these fitting loss coefficient values include any
static pressure gains or losses that may occur at
various flow conditions. A loss coefficient with
a negative number (-) indicates a regain, and a
value with a positive number (+) represents a
pressure loss, The designer should not use any
additional regain values, other than the ones
indicated in the fitting loss coefficient tables,
when performing friction loss calculations.
This completes the discussion of duct sizing
methods, You should now complete Quiz II to
test your knowledge of these concepts
Commercial Duct Design
26WORK SESSION |
EQUAL FRICTION DUCT DESIGN
We will now put to use some of the skills that we have learned thus far to size a duct system using the
equal friction method.
ven:
The fast food restaurant shown below will be served by three packaged rooftop units. For this example
‘we will only be designing the 12-1/2-ton duct system serving the South exposure seating area.
Unit airflow rate: 5,000 CFM Supply duct connection size: 14" x 28"
Supply diffuser pressure loss: 0.10 in. w.g Return duct connection size: 12"x 36"
Return air grille pressure loss: 0.06 in. w.g.
Task 1: Size the supply and return duet system using galvanized sheet metal duet with a 2" spray-
coated liner on the main supply and a 1" spray-coated liner on the return duct, Use pre-insulated flex
duct for the branch duct runs. Use a design friction rate of 0.10 in./100 ft. E.L.
Task 2: Determine the total static pressure loss for both the supply and return duct systems.
FAST-FOOD RESTAURANT
3 ‘Commercial Duct DesignWORK SESSION DUCT LAYOUT
FAST FOOD RESTAURANT
;
os | cls
1 | ef
S ar ee a @
C2] 0D] rettentn
Not To Scale
‘Commercial Duct Design 4WORK SESSION I!
STATIC REGAIN DUCT DESIGN
We will now work through a static regain example to illustrate the differences in the two methods,
Refer to the example problem in Work Session I.
Task 1: Size the supply and return duct system using the static regain method, Compare and contrast
the results with the equal friction method used in Work Session I.
35 ‘Commercial Duct Designrz eS a SE
APPENDIX,
Chart 1 — Friction Loss Chart for Round Duct
Table 1 — Circular Equivalent Diameter, Equivalent Area, and Duct Class of Rectangular Ducts for
Equal Friction
‘Table 2 ~ Recommended Maximum Duct Velocities for Low Velocity Systems (FPM)
‘Table 3 — Velocity Pressures
Table 4 Duct Roughness Multipliers
Table 14—SMACNA Fitting Loss Tables
Duct Design Sizing Worksheet
Equal Friction Example Worksheet
Static Regain Example Worksheet
Quiz I Solutions
Quiz Il Solutions
Work Session I Solution
‘Work Session II Solution
References
‘Commercial Duct Design 36SSS EE eee
FRICTION LOSS CHART FOR ROUND DUCT
loonco SA SO ols 93, 4 GBcs ow 19 ts 2 30 80 89855566
rooo0 [> A 7 70.000
0000 | 50000
40000 0009
20000 20000
15000, 1.000
000 000
+5000 000
3 4000 4000 =
& 000 sooo ©
5 500 vs00 2
500 200
00 800
300 300
200 200
160 180
s0 80
"ogo oF 506 08 1 OB Of 03 Ga asas as Wi to 40 Wo e040"?
FRICTION LOSS (IN. W6 PER 100 FT OF EQUIVALENT LENGTH}
CHART 1
37 Commercial Duct DesignTABLE 1—CIRCULAR EQUIVALENT DIAMETER,” EQUIVALENT AREA AND DUCT CLASS}
‘OF RECTANGULAR DUCTS FOR EQUAL FRICTION.
= a 1° @ we
0 [ine Dicw |Are Diem [Aves Dion [Ang Dian [Area Diam [Ares Dion [Arce Diam [Area Dizm | Area Disem
foe ae |e i ane Pia | Pia” | ath Pin” |e Pin |S Pin” [ay in” | eat Ti
wo | ar ea| sea] os 108
ve | 298] mas or aw] roe tara 39
waa a7 fae asa [ias tea [ver as
size lias ses [ia Ago] res a7a}tarss|aaa wr
ois {tae rsa [re den[ tar ina|aor s9s|238 aor| 2s 219
von sar|tse59|ta2 ize [to 10a |aar2oa|asr 27 [zee aa | air 24
Py Vie tas [tao sean aie tsalzar aia [am aa lam 239/342 2s.
En 1a aae iat va| ie tala ma |aas mar [sey ass [ass aa art ast
2 va ass [wigs wz [am —ivalaar via |aes azo [as aee aso 287 [aon ar
x0 Ta jer |te2 qalam doa|aee 20 [306 a7 fsae” asa]asy ae7|aay a0
2 Tie jes [toscaha|aae doa|ze 97/325 tee] an colar ars[ass 209
ae [uss sae [ise ara 20s —malauy ara 296 203 ]348 ass]ae0 267] ear malear m7
ae fis ivy fies ira [ate toa taar —aiv]an a9 [sus ase] 400 ara| ase 20] 507 305
ae {iss iso fis raja a0a]are 22s |aar 245 [390 264/490 ras lane 2a| sar 31
tar 18a |2a8 207|aea 230 aaa a1 /ae7 rol as 288 | S07 sat
a tae is |zes2is|n9e anal asr ase[aas ars[ ar a0a| sar oa
Me [tae iso [iss ane [asa aes|aar 2s9|az1 20s ass 2x2 |4s0 so | 555 as
qe fias tea |20r 9a [aa aro aaa aas|aan er] ae 287 (510 208/576 34a
ae [ise tes|200 sean a23|aas 2e8/ aos w72|aes 292/530 912/597 a3
0 brs i99|aer727[aa6 asa|ars za [ ase 29a | sat 318/619 a5
” aa m2 |291 asi|aarase|4a0 das |soo- dos | azz salons 360
se aus wos|2ee zal 261|4as 2s | sir 305| 390 329/604 bea
se 230209 [noe 23s[ aaa 265/455 209 | sar 22 | ean 334/687 ma
se aaa ait |aay 22 ]a94 aso | ase wea [sas azz | 026 39/ 706 30
ro aso at|aar 245/406 27a] aoe wal sas 322/050 345|726 ass
o des 220 |saa 252/424 a79| 810 906/81 321 | ear 355/770 mr
aaa aca] aan 207] sar ara | eae av9|7an aca] aa wr
n ner 2es[ar) aoa| sas 323/600 Mal 7se or aa
% top ara [ao o00| 56 s2a|eas sal 79s 382 aa
ra ais wel sir sa Rajya 364 wolea afta a8
" say ns Ses] 7s 32 inal ors zs|t08 see
4 seu 30 sea | 7a7 30 as[tor ala ase
7 s26/eo1 ase]ain sas] oae ais|t04 wal nn7 460
oy S90 50/714 aca ea 392/970 au lioa as| 121 «72
10 yao 309/850 ms|omo aas[na 4ss| 29 ae
0% 740 a7aleg aos| toa aas[us wa] 190 aa
108 720 3s0|920 412/106 440/120 Wola we
a tio ase|es0 ara] tos a7| ta a75| 198 903
We su aap via ass) a6 aes faa 51a
10 too wel is asolia wtlrea sts
m4 wos as| 19 467/194 elise S24
we vipa #i[ne wales 9
wa ns 79/14 so3] ise 530
16 tae ans| 14s ste | 16a 54s
wo 130 wea| a7 20] tas S50
Me ta walisa 529] 168356
“hese epdraln dane) Caled tom a = 1 ‘are rambled i.
i.e a= a en rs
Commercial Duct Design 38SEES eee
TABLE T—CIRCULAR EQUIVALENT DIAMETER,* EQUIVALENT AREA AND DUCT CLASS}
OF RECTANGULAR DUCTS FOR EQUAL FRICTION. (Cont.)
” 3 2 Ey * 36 = 7
08 [ares Diem [Area Dias [Aree Dior fara Dina
[Arse Diam [Aree Diem [Area Diam [Ares Din
sate Tin” [tae Sim” [tae in [eet Pin
sett Tin” [rit “im [etn Sin” [Aare
24 [a70 362
26 [40s ara lam 254
soi lsar_sia|s79 mae |aas 398 [ase 50
ae [sas sta [sae aa fas 3a [706 360 [rsa a
36 [588 220/594 30/432 sus |ao 35 |ras sro |yas sez leas 394
a zaleae 042 /er 353 |ra0 a7 [per seo |nar et |een aod|oaa ane
So [EE Relat ea [rm sea ry ee lease lata |vae ata] oan eae fos an
4a [eas sea] 703 59 |758 37.3 |arde gee [ass me |oa1 sii|seo waa|ton aae|ine cae
aa [67s 382] 734 67 |70 301 [sso 395 [sor ana |ver az (toa aas|qoa aee|tia ee
46 [70s asa /70a azaleas sao leas wos
aa [730 6s] 798 ana ser|eas ua
‘eafior wa[naae[ne aa
eo}a gana ass|aa ae
so | x50 389 wos|ser eo aslns wilma ia|i90 ase
32 |zar 36 |oas aia |ome ae ala. oalar aaa 07
sa ‘aloe woltea ae 4is|i6 ol na 2 [ine soa)
ae
aa|9o a7 [ror aa asa|ia a7a|i30 ass|ta7 sod [tas a1
so fea alors slios olna ase 3/109, oa) us srliss 533
os [om uslvoa wslna alia 72 a7 lia szo| ss sra| ies a0
oo [os aslto 7 na 4e|iz8 ssa sas|ts saws saa
na jis aslns wolfe galiss 7 509 sos|vaa sa@
7 {wa 43/0 golia ola sos 563 sra|i9a 395
eo fins asa a0 sou [1a a0 78 wa] ma ein
fio aes sa sna 589 wor|na ea
ns 9, 4 oo eal m1 637
as ay sna a w2|n0 «0
“6 Sa sso) 7a sol ies sas eas es\ ase 685
ms a 548 ssa|ia soa 37, ws|zs 7
1st sr ass sea|i97 os eral sy a7 [am 705
rr wea [ma ari fazo wefan as7) aan ars] 262
wo fiz 4s ot exo lar wes|242667| ae apa] 272
seilies“es[21¢ exo [m2 se|as2_oea| ae ora] 202
sealz0aot1[m2a ea |ts7 oso ase ana|a7a roa] 207
ss|208 o1t|m26 age |0s aro |a6a ps | 202 720/298
alas 0a7|m0 ao lr1 @o{ ae 70a| 207 r26| 305
ne [tse s52
we [a seo
wa2_| ra 05}
wo [as sea “ro [a3 640/28 was |as9 elas rtalara 735] aus
ta [re sar] 206 ors | any ces ran 75 [26a ons|262__p20[ a0 7a| 320
“Cheam! dance Clad em as = 13
‘Hore tn nab re dc Zen
39 Commercial Duct DesignTABLE 1—CIRCULAR EQUIVALENT DIAMETER,” EQUIVALENT AREA AND DUCT CLASS}
‘OF RECTANGULAR DUCTS FOR EQUAL FRICTION. (Cont.)
str
Salma ts [ina 75)
Be Sing les
\gea\ees|zaeirs
ia ss fea|ann a] ee ste fe
rar on mtr) Caled om = 13
Commercial Duct Design 40SSS ee
TABLE 2—RECOMMENDED MAXIMUM DUCT VELOCITIES FOR LOW VELOCITY SYSTEMS (FPM)
SanRGline Fete ‘CONTROLNG FACTORDUCT FRICTION
APPLICATION NOISE GENERATION, Mein Duets
is Bor Supply, ‘Return Supply [Return
Roden a 0 200 7 609,
“Apartments |
Atal Bogrooms 000 100 1300 100 1000
Hospital Bedrooms |
Frito Often
Draton Boom 1200 2000 1500 1400 1200
Ketone 00 1300 00 1000 300
General Officer
High Clot Retourons 7
Hie cl te 500 200 1300 1400 1200
Senks
tee 00 2000 1800 1400 200
Indu 2500 3000 100 700 700
TABLE 3—VELOCITY PRESSURES
vetocry | vetocty | vaoery | veocny | vaoery | vocry | vaocry | veocmy
pressure | (r/min) | pressure | iei/min) | pressure | “faymint | raeseune | “spares
ina) ‘in wa) ine we) ins wal)
or 0 3 Tiss 3 7055 a3
02 ses 30 aio r 300 eo
om ies ey ino 3150 a0
7 ry ey 20 i200 rao a0
as a5 2 B00 3280 va i200
6 980 2330 00 Tae 70
or 1080 270 ss0 tsa 2930
8 1130 200 590, 136 ‘000
9 1200 ao 340 v80 000
i 170 2070 3499 Nee 3190
a 2500 3590 1a 3190
12 2530 3880 in 3250
3 2500 3420 176 Siro
a 2590 3470 va0 Smo
ns 380 710 Kee 5630
6 7650 750 7 $490
7 2830 379 1 3550
‘ zo ano 136 +5600
3 ino 3ae0 200 3560
20 70 3020, be sro
2 7300 Th60 208 970
2 2830 co an 3230
2 iso toe ‘eo aie
a 280 vo8 eo 2m
a a0 aa 23 24
26 2940 Te “a1 ae
2 ar 120 38
290 um us
NOTES: T Bato for aandard ar (2992 mn Hg ana 70 FL
2. Dota derived tom the following eavoton (aa) MY a tm
> Coos he = pres diferance termed “veloity head” in wo!
41 Commercial Duct DesignTable 4 — Duct Roughness Multipliers
DUCT MATERIAL ROUGHNESS MULTIPLIERS
For internal ductwork surfaces other than smooth sheet metal,
multiply equivalent lengths by:
MULTIPLIER
SUPPLY RETURN
DUCTWORK DESCRIPTION
Rigid Fiberglass — Preformed Round Ducts — 1.0
Smooth Inside
Rigid Fiberglass Duct Board 4.30
Duct Liner — Airside Has Smooth Facing 4.30
Material .
“Flexible Metal Ductwork (Straight Installation) 1.6
Duct Liner — Airside Spray-Coated
“Flexible, VinylCoated Ductwork with Helical
Wire Core (Straight Installation)
INSTRUCTIONS: Multiply the measured length of each section by the appropriate
multiplier to calculate the total footage equivalent to the same
friction loss in smooth sheet metal ductwork.
*Flexible duct multipliers assume that the duct is installed fully extended.
‘Commercial Duct Design aSMACNA FITTING LOSS TABLES
TABLE 14
Reprinted by permission of SMACNA.
8 ‘Commercial Duct Designia DUCT DESIGN TABLES AND CHARTS
‘Table 14-10 LOSS COEFFICIENTS, ELBOWS (Cont)
Use the velocity pressure (V,) of the upstream section. Fiting loss (TP) = © x Vs
D. Elbow, Rectangular, Mitered (15)
CCoatcentC (Soe Note 2—Page 14.19)
ww
as [os [ors [40 | 18 | 20] 30 | «0 | so ao
ze | 008 | 008 | 00s [oor | oo7 | 007 | 008 | 008 | 005 005
go: | ove |Oy7 | os7 [ose | ors | avs | oa | 079 | 12 ont
as | oe | 037 | 030 foe | 033 | os | 028 | o27 | ozs Ope
bo | deo |osa | os7 oss | 082 | 040 | o4s | 04s | ot 038
Bet | 097 | 073 | O67 | oss | v6 os?
42 fut | ta | 099 | 092 | 089 bas
SN oo |S [Sy [a
E. Elbow, Rectangular, Mitered with Converging or Diverging Flow (15)
© (Sse Note 2—Page 14.18)
ww -
lw. oa [12 [1] 16 | 20
1a ta fa faa
44 | to | as | 090 | ob
44 [om ave | o72 | 066
v0 [069 | 06s | oo | oss
F. Elbow, Rectangular, Smooth Radius without Vanes (15)
CCoeticionts for 80" etbows: (See Note)
Cooticient & (5
rw _ -
035 [os [076 30 [40 | $0 | 60 | 00
os [1s [14 | ia F vo fur par [az | az
875 | osr |os2 | 04a | O44 | O40 038 | o40 | o42 | 043 | 048
1 | o2r |o2s | os | 021 | ore ‘18 | 038 | 020 | 027 | oat
15 | 022 | 020 | one | o17 | 015 ox4 | os | 0.46 | 017 | 017
20_| 020 | 018 | ox | ons | 014 043 | ate | 084 | 04s | 035
Raw . M
TT2]Ts]* [ses [ee] ©] «| ao
ao | 326 [vas | aaa | so | vos | soe | vo |
co | 97 | vee | vse | tae | 138 | to | 5] to
os [a
207s _| 2)
us. unite
ForStandard Air: (Metric Units)
= 8580V (R= 684 0V)
eee
= Get amt. ichos (rm)
1 dct eta, pm rs)
For Rectangular Duets
aN
De ae
ew
‘Commercial Duet Design 44‘Table 14-11 LOSS COEFFICIENTS, TRANSITIONS (Diverging Flow)
Use the velocity pressure (V,) of the upstream section, Fitting loss (TP) = C « Vy,
A. Transition, Round, Conical (15)
US. Units (Met Units)
R-assov (A, 66.4 Dy)
nore:
= Upstream Oiamete: ches (mm)
= Upsteam Voc. pm t's)
Costciont G (See Note 6)
2
R fa — —
1@ | 20 | 30 | ae [ or | a0 | 100 | 100
05 8 10 2 aia | 019 | a32 1 033 | 033 | 022 | 031 | 030
4 |ozs | 020 | ove | og | ass | 064 | ces | oes
& [oar | aay | oa | oes | avr | on | os | ove
10 [029 | 038 | os | o76 | oa | 099 | oes | ona
21s ost | ose | oso | oa oe | oes | oon
2 2 [oor [ov | 023 | o2e oar | az | oa
4 Joss | ois | 035 | 055 | 089 | 099 | ose | oer
& Jars | ozs | oss | os | a70 | or | on | oes
19 |.020 | 024 | o43 | o76 | 000 | om: | oat | oe
218 [02s | ozs | ose | 076 | oar | obr | os7 | oar
Ox 10 2 [eos | oor | ov | oar | oar | oar | oar | oz
4 for | 024 | oss | os | ose | 058 | ose | oar
5 Jars | 029 | 0x6 | og | og | a7 | 070 | 07
x0 Jozi | 033 | ose | os | ove | 40 | oes | cas
216 |oz | ose | 06 | are | ors | oes | oer | ono
'B. Transition, Rectangular, Pyramidal (15)
ts 4
Wren e = 100"
Costicion¢ (See Note 6)
Wa.
we [wo [oe |e] @ | oo | ee | ier
2 038 | 022 | 02s | o29 | or | oa | 038 | 030
4 gas | cas | oso | 086 | oe: | 089 | oss | 009
5 oa | o47 | oss | oss | ov | ove | ore | O78
210 ose | 04a | oss | a7 | 000 | oar | oes | oe
~ Aten (Entering sirsteam), Ay = Area (Loaving airstream)
45 Commercial Duct DesignTable 14-11 LOSS COEFFICIENTS, TRANSITIONS (Diverging Flow) (Cont.)
Use the velocity pressure (V,) of the upstream section, Fitting loss (TP) = C x Vo
G. Transition, Round to Rectangular (15)
vaso
7
For Figures and 0, compute using the
‘Sauaters and id thacoaicer Grom
“abe 14-18, Tanaon. Retangvax, rami.
. Transition, Rectangular, Sides Straight (15)
In
. le | [= | | |
2 ooo] 012 | 020 | om | as | ose | oss
‘ oie | 02s | 042 | 060 | oes | o7 | 006
6 oi | oo | oa | oss | ove | om | om
F. Transition, Symmetric at Fan With Duct Sides Straight (15)
Coaticiont © (S00 Note 6)
avA [15 | 20 | 25 | 30 | 38 [40
RIK 051010
A,
a Fat ie ct (te trends op)
‘Table 14-15 LOSS COEFFICIENTS, ENTRIES
Use the velocity pressure (V,) of the downstream section. Fitting loss (TP) = G % Vp
‘A. Duct Mounted in Wall, Round and Rectangular (15)
i =o |osolosr [ose 092 | 10 | 10
@NE wm 2t[23 [28 (8% [23 [888 [33 [8m
s annem Pee
WESTER ISTE +
Rectang = BEN by, Thick Edge (UD, > 0.05):C, = G + Gy
Cs new oofiet of sng wih a Sreen or peroato pat tthe etrance
i tom above abo
i em Tabi 16-72 (screen) or Table 4-178 (pedrated plete)
Note 8:4 = Area.Q ~ Alon V = Vaocty
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‘Commercial Duct Design
3WORK SESSION I - SOLUTION
It is recommended that you initially work through this example using the tables in the Appendix so that
you gain an understanding of the design process. In the future you may wish to use a duct sizing
rule or wheel-type device (See Duct Calculator reference) to simplify calculations and reduce the time
required for sizing,
Since all required information is given, enter the known values on the Duct Design Sizing Worksheet.
The supply duct layout is symmetrical, meaning that we only have to size one half of the duet system,
then we can use the same sizes for the other side.
Note: Table references below refer to the tables in the Appendix.
Supply duct:
Step 1: The first thing you should do is label all duct sections and nodes. A node is @ point in the duct
system where there is either a change in airflow quantity or @ change in airflow direction (examples
include a fitting, elbow or a piece of equipment such as a diffuser or grille). A duct section begins and
cends between node points, Use whatever labeling convention you want; however, it is suggested that
you use a combination of letters and numbers so you don’t confuse them. In our example we will label
nodes with letters and sections with numbers.
Examining the duct system layout, we can see that the duct run with the greatest friction loss will likely
be either from the fan to node “F” or from the fan to node “O”. Since the duct system is symmetrical,
the friction losses should be identical for both of those duct runs, Let’s size the duct sections on duct
run (fan-F) first, then come back and size the other sections afterward.
Step 2: Choose an initial velocity from Table 2 in the Appendix. Since this type of environment is not
likely to have stringent sound requirements, let’s select the initial velocity at 2,000 fpm corresponding
to a cafeteria. The supply duct connection size is given as 14" x 28". Since we have a “tee” fitting
directly below the unit that splits the airflow, we need to transition from the unit duct connection to
more of a square shape since most “tees” are not built with an aspect ratio of 2.0. Let’s try a 24” x 24"
transition, Remember, however, that there is 2” of duct lining in the supply duct, therefore all metal
dimensions will need to be increased by 4" to accommodate the lining. After you select the appropriate
airflow dimensions you should then add for the duct liner. Go ahead and enter the transition as the first
element on the duct sizing worksheet.
Now we need to determine the transition fitting loss, From Table 14-11 there is @ type “B” fitting that
‘meets our requirements, The table of C-values requires us to know the ratio of inlet and outlet areas. It
is calculated as: (Ay/A) = [(24" x 24") / 14" x 28")] = 1.47, The smallest value of (Ay/A) in the table is
2.0, so let's use that and assume that the transition angle is 30°. Read the C-value as 0.25, Since itis a
diverging-type fitting, we need the velocity pressure upstream of the fitting in order to arrive at the
fitting loss. Find a 14” x 28" duct in Table 1 and read the diameter as 21.3. From the friction chart at
21.3" diameter read the velocity of approximately 2,050 fpm. The velocity pressure is: (2,050/4,005)* =
26. Add this value to the worksheet and multiply by the friction rate. Therefore, TP = C x Vp = 0.25 x
0.26 = 0.065 in. w.g. Add this value to the worksheet.
Commercial Duct Design 60Step 3: Section | will be the first section of straight duct off the fan. The length is given as 2 ft. Since
the problem states that we are using spray-coated duct lining, we need the material roughness factor for
it, From Table 4 read this as 1.9. Let's check our 24" x 24” duct and verify our velocity. We now work
backwards from the rectangular duct dimension table (Table 1) and determine the round duct
equivalent. Find a 24" x 24” duct and read the equivalent round diameter as 26.2". Now, using the
friction chart, find the intersection of the round diameter with the airflow quantity (5,000 CFM). Read
the friction rate as 0.10 in. w.g. / 100 ft. E.L. and the round duct velocity as 1,400 fpm. Enter the
dimensions for duct section 1 on the worksheet, Next we need to determine the section friction loss.
Multiply the friction rate by the material correction factor and the length to determine the friction loss;
0.10 x 1.9 x 2/ 100 = 0,004 in. w.g. You can calculate the velocity pressure or read it from the friction
chart. You will need this information later to calculate the fitting loss associated with the “tee”. The
velocity pressure is (1,400/4005)" = 0.122 in. w.g.
Step 4: Since the problem did not state which fitting types to use, we will have to select appropriate
ones from Table 14. We have a symmetrical “tee” fitting that splits the air equally. From Table 14-10
we find a type “L” fitting, To arrive at the appropriate “C” value, we need to know the “W" and “I”
values. Since these values are dependent on the size of the next duct sections (sections 2 and 8), and we
haven't yet sized them, let's skip the “tee” fitting calculations for now. We'll come back to it after we
size duct sections 2 and 8. Go ahead and list the “tee” fitting as the next element on the worksheet,
Step 5: Let's proceed to section 2, which begins at node C and ends at node D. Now is a good time to
sum the airflow values, starting at the terminals and working back toward the fan. Go ahead and write
the CFM values on the duct layout diagram next to the section numbers. Section 2 has an airflow
quantity of 2,500 CFM. Using the design friction rate of 0.10 in. w.g. / 100 fi. E.L. find the intersection
point with the airflow rate, This corresponds to a round diameter of approximately 20 in. Next find a
combination of rectangular duct sizes in Table 1 with a diameter of approximately 20 in, A 20" x 16"
duct has an equivalent round diameter of 19.5". From the friction chart find the corresponding velocity
of 1,200 fpm. Enter these values and complete the section friction loss calculations.
Step 6: Now that we know the size of section 2 we can go back and finish the fitting loss calculations
for the “tee” fitting. Refer to Step 4 above. The note for Fitting type “L” says to use a similar elbow.
Let’s use a type “D”, which is a 90° mitered elbow without turning vanes. The H/W ratio is: 16/20 =
80. From the table read the C-value as 1.2. The fitting loss may now be calculated as: Tp = 1.2 x 0.122
= 0.146 in, w.g.
Step 7: Next we come to a branch fitting with a round tap off'a rectangular main at node D, Referring to
the fitting loss table, we find a type “I” fitting in Table 14-14, Notice the table is labeled “Branch
Coefficient” which means the table includes C-values associated with the branch duct section only.
There is a note that says, “For Main Loss Coefficient see Fitting 14-14”, Since we are first sizing the
Jongest duct run (fan-F) we will need the “Main” loss coefficient now. Later we will need the “Branch”
loss coefficient for calculating the branch duct fitting losses at nodes D, E, L, and P. Refer to fitting
type “A” for the “Main” loss value, From the table we need the ratio of velocities Vs / Ve, however we
don’t yet know the velocity of the next section (section 3) because we haven't sized it yet. Add the
“tee” fitting to the worksheet and let’s skip the fitting loss calculations for now until we complete the
straight duct section sizing.
61 ‘Commercial Duet Design