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a b l e 2. C ir c u l a r E q u iv a l e n t s of R e c t a n g u la r D ucts fo r E q u a l F r ic t io n a n d C a p .T Dimensions in Inches ;:'
676
CHAPTER 31
1952 Guide
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Air Duct'Design
677
tKe air; and are therefore conveniently expressed as a fraction of the:velocity
head:
' U : -.9.;.::;..;.
h. (4)
and for standard air
where
hy = dynamic pressure loss, feet of fluid flowing. , Hv = dynamic pressure loss, inches of water.
v = velocity of fluid, feet per second:
:;<s)
Fig. 4. Relation Between Velocity and Velocity Head for Standard Air
f ^ = the velocity pressure corresponding to the mean velocity of flow, feet of fluid
flowing.
.j -
.;
- ...,: , ; ' .
V = mean velocity of standard air, feet per minute.
. j,,,..
C = an experimentally determined constant (dynamic loss coefficient). , . ,
It can be seen from Equation 4 that the dynamic loss coefficient is' inde pendent of both density and the units used, and that it representa 'the number , of velocity heads lost at the conduit transition or bend. Yalues of the dynamic loss coefficient for various duct elements are sometimes
tabulated,'7- * though it should be kept in mind that absolutely: reliable dynamic loss coefficients have not yet been fully established;, for all duct
elements.
...
,
Fig. 4, which shows the relation of velocity pressure to velocity for stand
ard air (Y = m5VHy), can be conveniently used to find the total dynamic pressure loss for any duct element with known dynamic loss coeflikent C. This coefficient is nearly independent of the air velocity and the roughness of the duct walls; therefore dynamic losses cannot theoretically be computed as friction losses. For duct components where intense eddying flow is not
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