B. OTHER FACTORS AFFECTING DUCT SYSTEM PRESSURES
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CHAPTER 5
Figure 56 CHANGES FROM
"SYSTEM EFFECT" (1)
during high winds. Supply and exhaust systems, and
openings, dampers, louvers, doors, and windows
make the building flow conditions too complex for
most calculation. The opening and closing of doors
and windows by building occupants add further complications.
Mechanical HVAC systems are affected by wind conditions. A lowpressure wall exhaust fan, 0.05 to 0.1
in w.g. (12 to 25 Pa) can suffer a drastic reduction in
capacity. Flow can be reversed by wind pressures on
windward walls, or its rate can be increased substantially when subjected to negative pressures on
the lee and other sides, Clarke (1967) when measuring HVAC Systems operating at 1 to 1.5 in. [w.g.
(250 to 375 Pa), found flow rate changes of 25 percent for wind blowing into intakes on an Lshaped
building compared to the reverse condition. Such
changes in flow rate can cause noise at the supply
outlets and drafts in the space served.
For mechanical systems, the wind can be thought of
as producing a pressure in series with a system fan,
either assisting or opposing it (Houlihan 1965).
Where system stability is essential, the supply air and
exhaust air systems must be designed for higher
[pressures about 3 to 4 in. w.g. (750 to 1000 Pa)] to
minimize unacceptable variations in flow rate. To conserve energy, the system pressure selected should
be consistent with system needs.
Where building balance and minimum infiltration are
important, consider the following:
a) Fan system design with pressure adequate to
minimize wind effects.
b) Controls to regulate flow rate or pressure or
both.
c) Separate supply and exhaust systems to serve
each building area requiring control or balance.
d) Doors (possibly selfclosing) or doubledoor air
locks to noncontrolled adjacent areas, particularly outside doors.
e) Sealing windows and other leakage sources
and closing natural vent openings.
5.7
DUCT
DESIGN
FUNDAMENTALS
3. Stack Effect
When the outside air is colder than the inside air, an
upward movement of air often occurs within building
shafts, such as stairwells, elevator shafts, dumbwaiter shafts, mechanical shafts, or mail chutes. This
phenomenon, referred to as normal stack effect, is
caused by the air in the building being warmer and
less dense than the outside air. "Normal stack effect"
is greater when outside temperatures are low and
when buildings are taller. However, "normal stack effect" can exist even in a one story building.
When the outside air is warmer than the building air,
a downward airflow frequently exists in shafts. This
downward airflow is called "reverse stack effect." At
standard atmospheric pressure, the pressure difference due to either normal or reverse stack effect is
expressed as:
Figure 57 PRESSURE DIFFERENCE DUE TO
NORMAL STACK EFFECT (2)
Equation 55
Where:
Ap  pressure difference, in w.g. (Pa)
To
absolute temperature of outside air, R (K)
T1  absolute temperature of air inside shaft, R (K)
h= distance above neutral plane, ft (m)
ks
coefficient, 7.64 (3460)
For a building 200 ft (60 m) tall with a neutral plane
at the midheight, an outside temperature of 0 F
(  18 C) and an inside temperature of 70 F (21 C),
the maximum pressure difference due to stack effect
would be 0.22 in. w.g. (55 Pa). This means that at
the top of the building, a shaft would have a pressure
of 0.22 in. w.g. (55 Pa) greater than the outside pressure. At the bottom of the shaft, the shaft would have
a pressure of 0.22 in. w.g. (55 Pa) less than the
outside pressure. Figure 57 diagrams the pressure
difference between a building shaft and the outside.
In the diagram, a positive pressure difference indicates that the shaft pressure is higher than the outside pressure, and a negative pressure difference
indicates the opposite. These pressures would affect
all HVAC systems operating throughout the spaces.
Stack effect usually exists between a building and the
outside. The air movement in buildings caused by
both normal and reverse stack effect is illustrated in
Figure 58. In this case, the pressure difference expressed in Equation 55 refers to the pressure difference between the shaft and the outside of the building.
5.8
Figure 59 can be used to determine the pressure
difference due to stack effect. For normal stack effect,
Ap/h is positive and the pressure difference is positive, above the neutral plane and negative below it.
For reverse stack effect, Ap/h is negative and the
pressure difference is negative above the neutral
plane and positive below it.
In unusally tight buildings with exterior stairwells, reverse stack effect has been observed even with low
outside air temperatures (Klote 1980). In this situation, the exterior stairwell temperature was considerably lower than the building temperature. The stairwell was the cold column of air, and other shafts within
the building were the warm columns of air.
Note: Arrows Indicate Direction of Air Movement
Figure 58 AIR MOVEMENT DUE TO NORMAL
AND REVERSE STACK EFFECT (2)
CHAPTER 5
If the leakage paths are uniform with height, the neutral plane is near the midheight of the building. However, when the leakage paths are not uniform, the
location of the neutral plane can vary considerably,
as in the case of vented shafts. McGuire and Tamura
(1975) provide methods for calculating the location of
the neutral plane for some vented conditions.
changes in a duct system with the total pressure and
static pressure grade lines in reference to the atmospheric pressure datum line.
At any crosssection, the total pressure (TP) is the
sum of the static pressure (SP) and the velocity pressure (Vp).
Equation 56
TP = SP + Vp
C SYSTEM PRESSURE
CHANGES
1. Changes Caused by Flow
The resistance to airflow imposed by a duct system
is overcome by the fan, which supplies the energy (in
the form of total pressure) to overcome this resistance and maintain the necessary airflow. Figure 510 illustrates an example of the typical pressure
where:
TP = Total Pressurein. w.g. (Pa)
SP = Static Pressurein. w.g. (Pa)
Vp = Velocity Pressurein. w.g. (Pa)
In HVAC work, the pressure differences are ordinarily
so small that incompressible flow is assumed. Relationships are expressed for air at standard density of
0.075 lb/cu. ft. (1.2041 kg/m3), and corrections are
necessary for significant differences in density due to
altitude or temperature. Static pressure and velocity
pressure are mutually convertible and can either increase or decrease in the direction of flow. Total pressure, however, always decreases in the direction of
airflow.
2. Straight Duct Sections
For all constantarea straight duct sections, the
static pressure losses are equivalent to the total
pressure losses. Thus, for a section with constant
flow and area, the mean velocity pressure is constant. These pressure losses in straight duct sections
are termed friction losses. Where the straight duct
sections have smaller crosssectional areas, such as
duct sections BC and FG, the pressure lines fall more
rapidly than those of the larger area ducts (pressure
losses increase almost as the square of the velocity).
3. Reducers
Figure 59 PRESSURE DIFFERENCE DUE TO
STACK EFFECT (2)
When duct crosssectional areas are reduced, such
as at converging sections B (abrupt) and F (gradual),
both the velocity and velocity pressure increase in
the direction of airflow and the absolute value of both
the total pressure and static pressure decreases. The
pressure losses are due to changes in direction or
velocity of the air and occur at transitions, elbows,
and duct obstructions, such as dampers, etc. Dynamic losses can be expressed as a loss coefficient
(the constant which produces the dynamic pressure
losses when multiplied by the velocity pressure) or by
the equivalent length of straight duct which has the
same loss magnitude.
5.9
DUCT
4. Increasers
Increases in duct crosssectional areas, such as at
diverging sections C (gradual) and G (abrupt), cause
a decrease in velocity and velocity pressure, a continuing decrease in total pressure and an increase in
static pressure caused by the conversion of velocity
pressure to static pressure. This increase in static
pressure is commonly known as static regain and is
expressed in terms of either the upstream or downstream velocity pressure.
5. Exit Fittings
At the exit fitting, section H, the total pressure loss
coefficient may be greater than one upstream velocity
pressure, equal to one velocity pressure, or less than
one velocity pressure. The magnitude of the total
pressure loss, as may be seen in the local loss section, depends on the discharge Reynolds number and
its shape. A simple duct discharge with turbulent flow
has a total pressure loss coefficient of 1.0 while a
same discharge with laminar flow can have a total
pressure loss coefficient greater than 1.0. Thus, the
static pressure just upstream of the discharge fitting
can be calculated by subtracting the upstream velocity pressure from the total pressure upstream.
6. Entrance Fittings
The entrance fitting at section A also may have total
pressure loss coefficients less than 1.0 or greater
than 1.0. These coefficients are referenced to the
downstream velocity pressure. Immediately downstream of the entrance, the total pressure is simply
the sum of the static pressure and velocity pressure.
Note that on the suction side of the fan, the static
pressure is negative with respect to the atmospheric
pressure. However, velocity pressure is always a
positive value.
DESIGN
FUNDAMENTALS
discharge side of the fan, as demonstrated by Points
G and H (in Figure 510). The distinction must be
made between static pressure loss (sections BC or
FG) and static pressure change as a result of conversion of velocity pressure (section C or G).
8. Fan Pressures
The total resistance to airflow is noted by ATPsysin
Figure 510. Since the prime mover is a vaneaxial
fan, the inlet and outlet velocity pressures are equivalent; i.e. ATPsys= ASPsys' When the prime mover
is a centrifugal fan, the inlet and outlet areas are
usually not equal, thus the suction and discharge
velocity pressures are not equal, and obviously
ATPsys 5 ASPsys. If one needs to know the static
pressure requirements of a centrifugal fan, and the
total pressure requirements are known, the following
relationship may be used:
Equation 57
Fan SP = TPd
TPs  Vpd
(or as SP = TP  Vp)
Fan SP = SPd  TPs
where the subscripts "d" and "s" refer to the discharge and suction sections, respectively, of the fan.
Inlet and outlet "System Effect," due to the interaction
of the fan and duct system connections, are not
shown in this illustrative example, only actual system
resistances are shown.
9. Return Air System Pressures
7. System Pressures
There are many persons in the HVAC industry (and
elsewhere) that believe that return air in a duct system is "sucked back" by the fan; therefore the ductwork and fittings do not need the use of good design
practices (i.e. no turning vanes for mitred elbows, the
lack of smooth air flow into the fan inlet, the use of
"panned" joists in residential systems, etc.). How
wrong they are!
It is important to distinguish between static pressure
and total pressure. Static pressure is commonly
used as the basic pressure for duct system design,
but total pressure determines the actual amount of
energy that must be supplied to the system to maintain airflow. Total pressure always decreases in the
direction of airflow. But static pressure may decrease,
then increase in direction of airflow (as it does in
Figure 510), and may go through several more increases and decreases in the course of the system.
It can become negative (below atmospheric) on the
A diagram is shown in Figure 511 of a simple return
air system. Converting to absolute pressures, an atmospheric pressure of 14.7 psi or 407 in. w.g.
(101,325 pascals) at the inlet grille acts as a pressure
device (fan or pump) to PUSH the air through the duct
to the lower pressure end (404 in. w.g.100,575
Pascals) at the system fan inlet. The total pressure
drop of 3 in.w.g. (750 Pa) could be reduced substantially if the 90° mitered elbows had turning vanes and
the fan inlet connection was better designed. In reality, a return air or exhaust air duct behaves exactly
5.10
CHAPTER 5
Figure 510 PRESSURE CHANGES DURING FLOW IN DUCTS
Figure 511 RETURN AIR DUCT EXAMPLE
5.11
DUCT
as a supply air duct with atmospheric pressure pushing the air to the lower pressure area created by the
fan suction.
DUCT
D STRAIGHT
LOSSES
1. Duct Friction Losses
Pressure drop in a straight duct section is caused by
surface friction, and varies with the velocity, the duct
size and length, and the interior surface roughness,.
Friction loss is most readily determined from Air Duct
Friction Charts (Figures 141 and 142) in Chapter 14.
They are based on standard air with a density of
0.075 lb/cu. ft. (1.204 kg/m3) flowing through average
clean round galvanized metal ducts with beaded slip
couplings on 48 inch (1220 mm) centers, equivalent
to an absolute roughness of 0.0003 feet (0.09 mm).
The previous duct friction loss charts were based on
30 inch (760 mm) joints and an absolute roughness
of 0.0005 (0.15 mm), and most computer software
programs and duct calculators still contain these
older values. The SMACNA Duct Design Calculators
(both U.S. and Metric) contain the newer data.
In HVAC work, the values from the friction loss charts
and the SMACNA Duct Design Calculators may be
used without correction for temperatures between
50°F to 140°F (10 Cto 60 C) and up to 2000 feet
(600m) altitude. Figure 145 and Tables 1426 and
1432 may be used where air density is a significant
factor, such as at higher altitudes or where high temperature air is being handled to correct for temperature and/or altitude. The actual air volume (cfm or
I/s) is used to find the duct friction loss using Figures
141 and 142. This loss is multiplied by the correction
factor(s) to obtain the adjusted duct friction loss.
2. Circular Equivalents
HVAC duct systems usually are sized first as round
ducts. Then, if rectangular ducts are desired, duct
sizes are selected to provide flow rates equivalent to
those of the round ducts originally selected. Tables
142 and 143 in Chapter 14 give the circular equivalents of rectangular ducts for equal friction and airflow
rates for aspect ratios not greater than 11.7:1. Note
that the mean velocity in a rectangular duct will be
less than the velocity for its circular equivalent. Multiplying or dividing the length of each side of a duct
5.12
DESIGN
FUNDAMENTALS
by a constant is the same as multiplying or dividing
the equivalent round size by the same constant.
Thus, if the circular equivalent of an 80 in. x 26 in.
(2030 mm x 660 mm) duct is required, it will be twice
that of a 40 in. x 13 in. (1015 mm x 330 mm) that has
a circular equivalent of 24 inches (610 mm) diameter
or 2 x 24 = 48 inches (1220 mm) diameter.
Rectangular ducts should not be sized directly from
actual duct crosssectional areas. Instead, Tables
142 and 143 must be used, or the resulting rectangular duct sizes will be smaller creating greater duct
velocities for a given airflow.
E DYNAMIC
LOSSES
Wherever turbulent flow is present, brought about by
sudden changes in the direction or magnitude of the
velocity of the air flowing, a greater loss in total pressure takes place than would occur in a steady flow
through a similar length of straight duct having a uniform crosssection. The amount of this loss in excess
of straightduct friction is termed dynamic loss. Although dynamic losses may be assumed to be
caused by changes in area actually occupied by the
airflow, they are divided into two general classes for
convenience: (1) those caused by changes in direction of the duct and (2) those caused by changes in
crosssectional area of the duct.
1. Duct Fitting Loss Coefficients
The dynamic loss coefficient "C" is dimensionless
and represents the number of velocity heads lost at
the duct transition or bend (in terms of velocity pressure). Values of the dynamic loss coefficient for elbows and other duct elements have been determined
by laboratory testing, and can be found in the tables
in Chapter 14. It should be noted, however, that absolutely reliable dynamic loss coefficients are not
available for all duct elements, and the information
available for pressure losses due to area changes is
generally restricted to symmetrical area changes.
Tables 146 and 147, which show the relationship of
velocity to velocity pressure for standard air, can be
used to find the dynamic pressure loss for any duct
element whose dynamic loss coefficient "C" is
known.
CHAPTER 5
Equation 58
TP = C xVp
Where:
TP = Total Pressure loss (in w.g. or Pa)
C = Fitting Loss coefficient
Vp = Velocity Pressure (in. w.g. or Pa)
The velocity pressure (Vp) used for rectangular duct
fittings must be obtained from the velocity (V) obtained by using the following equation:
Equation 59 (U.S.)
Q
Where:
V = Velocity (fpm)
= Airflow (cfm)
A = Crosssectional Area (sq. ft.)
Where:
Vp = Velocity Pressure (in. w.g. or Pa)
V = Velocity (fpm or m/s)
Example 52 (U.S.)
An elbow in a 24 in. x 20 in. duct conveying 7000
cfm has a loss coefficient (C) of 0.40. Find the elbow
pressure loss.
Solution
Using Equation 59:
Using Equation 510:

.
N
Using Equation 58:
Equation 59 (Metric)
Where:
V = Velocity (m/s)
Q = Airflow (m3/s), 1000 I/s = 1 m3/s
A = Crosssectional Area (m2)
(or)
TP = C x Vp = 0.40 x 0.275
TP = 0.11 in. w.g.
(Elbow pressure loss)
Example 52 (Metric)
An elbow in a 600 mm x 500 mm duct conveying
3500 I/s has a loss coefficient (C) of 0.40. Find the
elbow pressure loss.
Solution
Using Equation 59:
Where:
V = Velocity (m/s)
Q = Airflow (l/s)
A = Area (mm2)
In fittings, such as junctions, where different areas
are involved, letters with and without subscripts are
used to denote the area at which the mean velocity
is to be calculated, such as "A" for inlet area, "Ac"
for upstream or "common" duct area, "Ab" for branch
duct area, "As" for downstream or "system" duct
area, "Ao" for orifice area, etc.
Velocity pressure (Vp) may be calculated from Equation 510 or obtained from Tables 146 and 147 in
Chapter 14.
(3500 I/s = 3.5 m3/s), (600 mm = 0.6 m),
(500 mm= 0.5 m)
V = 11.67 m/s
Using Equation 510:
Vp = 0.602 x (11.67)2 = 81.99 Pa (Use 82)
Using Equation 58:
TP = C x Vp = 0.40 x 82
TP = 32.8 Pa
Equation 510 (U.S.)
2. Pressure Losses in Elbows
Equation 510 (Metric)
Dynamicloss coefficients for elbows (see Table 1410) are nearly independent of the air velocity and are
affected by the roughness of the duct walls only in
5.13
DUCT
the case of the bends. In tables used in other texts,
the dynamic losses often are grouped with the friction
losses to facilitate design calculations by determining
bend losses in terms of additional equivalent lengths
of straight duct or inches of water. However, the elbow
loss coefficients in Table 1410 are used with the duct
velocity pressure to calculate the "total pressure"
loss of each fitting. The additional duct friction loss (if
any) of the elbow is included in the calculations for
the adjacent straight duct sections (by measuring to
the centerline of each fitting).
Data now available for losses in compound bends,
where two or more elbows are close together, do not
warrant refinement of design calculations beyond use
of the sum of the losses for the individual elbows.
Actually, the losses may be somewhat more or less
than for two bends. Loss coefficients for some normally used double elbow configurations may be obtained from Table 1410.
Loss coefficients for some elbows with angle bends
other than 90° may be computed from the table in
Note 1 on page 1419. Loss coefficients for elbows
discharging air directly into a large space are higher
than those given for elbows within duct systems (see
Table 1416 figure E).
DESIGN
FUNDAMENTALS
cient when the R/W ratio is equal to 1.0 or higher (see
Table 1410, figure F). However, most installations do
not have ample room for this configuration and
smaller R/W ratios are required The use of splitter
vanes drops the fitting loss coefficient values of these
low R/W ratio radius elbows to a minimal amount.
The splitter vane spacing may be calculated as
shown in Figure 512.
Example 53 (U.S.)
A 48 in. (H) x 24 in. (W) smooth radius elbow has a
throat radius of 6 in. Find the radius of each of two
splitter vanes and the fitting loss coefficient.
Solution:
Using Figure 512 and Table 1410, figure G:
From Table 1410. Figure G for two splitter
vanes, CR = 0.585
A. SPLITTER VANES
Smooth radius rectangular duct elbows (with radius
throat and heel) have a reasonably low loss coeffi
c) From the fitting loss coefficient table for two
splitter vanes (opposite R/W = 0.25), C = 0.04
1. Select the number of splitter vanes to be used
(1, 2 or 3).
2. Referring to Table 1410, figure G (Page 14.21),
calculate the R/W Ratio and select the Curve
Ratio (CR) from the proper table.
3. Calculate Splitter Vane Spacing (for the
number of vanes required):
Elbow with two splitter vanes
(Section View)
4. The proper fitting loss coefficient (C) can be
selected from Table 1410, figure G after determining the aspect ratio (H/W).
Figure 512 TO CALCULATE SPLITTER VANE SPACING
FOR A SMOOTH RADIUS RECTANGULAR ELBOW
5.14
CHAPTER 5
Example 53 (Metric)
A 1200 mm (H) x 600 mm (W) smooth radius elbow
has a throat radius of 150 mm. Find the radius of
each of two splitter vanes and the fitting loss coefficient.
Solution
Using Figure 512 and Table 1410, Figure G:
of the distortion created by some turning vane rails
(runners). But, multiple, single thickness turning vane
sections with vanes 36 inches (914 mm) long or less
can be installed in large elbows instead of using double thickness vanes.
2. Trailing Edges
Trailing edges shown on single thickness vanes, design numbers 1 and 3 in Figure 38 of ASHRAE 1989
Fundamentals Handbook Chapter 32 also have become an industry problem. SMACNA research has
shown that unless these turning vanes are made and
installed perfectly, trailing edged vanes, when made
with average workmanship, actually have a higher
loss than vanes without them. And when the vanes
are accidentally installed with the airflow reversed,
much higher losses develop.
c) From the fitting loss coefficient table for two
splitter vanes) (opposite R/W = 0.25), C =
0.04
B. TURNING VANES
1. Single vs Double Thickness
Duct fitting loss coefficient tables for elbows with turning vanes have been in earlier editions of the
SMACNA HVAC Systems Duct Design manual and
the ASHRAE Fundamentals Handbook (American
Society of Heating, Refrigeration, Air Conditioning
Engineers) since 1977 SMACNA research on duct
fitting turning vanes still indicates that using double
thickness turning vanes instead of single thickness
vanes, increases the pressure loss of elbows (see
new data in Chapter 14, Table 1410H).
Single thickness vanes have a maximum length of 36
in. (914 mm) as outlined on page 25 of the 1985
Edition of the SMACNA "HVAC Duct Construction
Standards." Turning vanes over 36 inches (914 mm)
are used in a double thickness configuration to keep
their curved shape with the higher airstream velocities found in some HVAC system ductwork and to
prevent vibration or fluttering. They are not more aerodynamic than singleblade vanes as originally
thought, as the loss coefficients in Table 1410H indicate.
Of course, there often are higher losses caused by
the shape of short, single thickness vanes because
Because of this research, the SMACNA Duct Design Committee has recommended that turning
vanes with trailing edges be eliminated from fitting loss coefficient tables and duct construction manuals when manuals are revised. They
have been eliminated from Table 1410H in this
manual.
3. Vanes Missing
For many years contractors, often with the system
designer's approval, have eliminated every other turning vane from the vane runners installed in rectangular mitred duct elbows. Some contractors even believed that they would lower the pressure loss of the
elbow by doing this. But they were wrong! This practice more than doubles elbow pressure losses, and
definitely is not recommended.
Figure 513 is a chart developed from SMACNAsponsored research performed by ETL Laboratories
in Cortland New York. ETL tested single thickness
turning vanes with a radius of 41/2 in. (114 mm). The
distance between vanes was varied from 3 in. to 61/2
in. (75 mm to 165 mm) in increments of 1/4 in. (6mm)
using embossed rail runners. Airflow velocities varied
from 1,000 to 2,500 fpm (5 to 12.5 m/s) in the 24in.
x 24in. (600 mm x 600 mm) test elbow. The loss
coefficient of 0.18 for the standard spacing of 31/4 in.
(82 mm) may be compared with the loss coefficient
of 0.46 at a 61/2 in. (165 mm) spacing (every other
vane missing). The pressure loss of the elbow with
missing turning vanes was over 21/2 times the pressure loss of a properly fabricated elbow containing
all of the vanes.
5.15
DUCT
DESIGN
FUNDAMENTALS
Figure 513 TURNING VANES RESEARCH
Example 54 (U.S.)
In a 2in. wg. pressure HVAC duct system that has
six 90° elbows, an airflow velocity of 2,200 fpm, the
velocity pressure (Vp) for 2,200 fpm is 0.30in. w.g.
Calculate the pressure loss of the 6 elbows, a) using
41/2 in. turning vanes, single thickness, with all vanes
present (Table 1410, Figure H), b) with every other
vane missing (see Figure 513), and c) with 2 inch
double thickness turning vanes on 2.25 inch centers
(Table 1410, Figure H).
Solution
a) Single, Standard Spacing
The loss coefficient for a 90 elbow with 41/2 in.
single thickness vanes is 0.23. Using Equation
56:
TP = C x Vp = 0.23 x 0.30
TP = 0.069 in. w.g.
Loss for 6 Elbows = 0.414 in. w.g.
b) Single, Every Other Vane Missing
From Figure 513, C = 0.46
TP = C x V, = 0.46 x 0.30
TP = 0.138 in. w.g.
Loss for 6 Elbows = 0.828 in. w.g.
5.16
c) Double, Standard Spacing
The loss coefficient for the 2 in. double thickness vane is 0.50 (2000 fpm).
TP = C x Vp = 0.50 x 0.30
TP = 0.15 in. w.g.
Loss for 6 Elbows = 0.90 in. w.g.
Example 54 (Metric)
In a 500 Pascal pressure HVAC duct system that has
six 90° elbows, an airflow velocity of 11 m/s, the velocity pressure (Vp) is 71.6 Pa. Calculate the pressure
loss of the 6 elbows, a) using 114 mm single thickness
turning vanes (Table 1410, Figure H); b) with every
other vane missing (see Figure 513); and c) with 50
mm double thickness turning vanes on 56 mm centers. (Table 1410, Figure H, No. 3).
Solution
a) Single, Standard Spacing
The loss coefficient for a 90° elbow with 114 mm
single thickness vanes is 0.23. Using Equation
56:
P = C x Vp = 0.23 x 71.6
TP = 16.47 Pa
Loss for 6 elbows = 98.82 Pa
CHAPTER 5
b) Single, Every Other Vane Missing
From Figure 513, C = 0.46
TP = C x Vp = 0.46 x 71.6
TP = 32.94 Pa
Loss for 6 elbows = 1976 Pa
c) Double, Standard Spacing
The loss coefficient for the 50 mm double thickness vane is 0.50 (10 m/s).
TP = C x Vp = 0.50 x 71.6
TP = 35.8 Pa
Loss for 6 elbows = 214.8 Pa
The difference in losses of the three different turning
vanes in the same elbows becomes very important
to the energy conscious HVAC system designer who
only has 2.0 in w.g.(500 Pa) system static pressure
to work with. The a) single thickness vane elbows
used 0.414 in. w.g. (98.82 Pa) or 20.7 percent of the
available pressure. The b) elbows, with half of the
turning vanes missing, consumed 0.828 in. w.g.
(1976 Pa) or 41.4 percent of the system pressure.
The c) double thickness vane elbows used 0.90 in.
w.g. (214.8 Pa) or 45.0 percent.
Another turning vane problem occurs when a rectangular duct mitred elbow changes size from inlet to
outlet. Until research data is available, the pressure
loss calculations should be based on the higher velocity pressure of the smaller size. The use of double
thickness vanes is not recommended because they
usually cannot be moved in many vane rails or runners so that they are tangent to the airflow. However,
the critical and rather common problem is that turning
vanes are put into the vane rails as they are for a
normal 90° elbow, as shown in Figure 514. Vanes
Figure 514 TURBULENCE CAUSED BY
IMPROPER MOUNTING AND USE OF
TURNING VANES
that are not tangent to the airflow direction can cause
a high pressure loss. This "nontangent to the airflow
problem" also happens in normal 90° elbows with
careless workmanship. A proper installation in a
changeofsize elbow is shown in Figure 515 where
the vanes have been installed so that they are tangent
to the airflow.
3. Pressure Losses in DividedFlow Fittings
A. STRAIGHTTHROUGH SECTIONS
Whenever air is diverted to a branch, there will be a
velocity reduction in the straightthrough section immediately following the branch. If no friction or dynamic losses occurred at the junction, there would be
no loss in total pressure and the change in velocity
pressure would be completely converted into a regain
(rise) in static pressure.
It has been found by tests that the regain coefficient
across a takeoff can be as high as 0.90 for well
designed and constructed round ducts with no reducing section immediately after the takeoff.
Under less ideal conditions, such as in rectangular
ducts with a high aspect ratio or takeoffs closely following an upstream disturbance, the regain coefficient can be as low as 0.50. A static pressure regain
of 0.75 normally is used. Static regain (or loss) is
included in the duct fitting loss coefficient tables which
have changes in crosssectional areas of the main
duct.
Figure 515 PROPER INSTALLATION OF
TURNING VANES
(Vanes do not have "trailing edges," but have been moved
in the vane runner to remain tangent to the airstream.)
5.17