- #1
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Trying to convert differential pressure (inch WC) measurements from a 6-inch diameter pipe into an air flow rate (cfm).
Here's what I got so far...
I'm assuming laminar, imcompressible flow with negligible friction, head, or thermal losses (this is a very low-flow system). From the Bernoulli equation...
V = (2P/d)^0.5
V = velocity
P = differential pressure
d = air density @ STP
area = A = pi(r^2)
flowrate = Q = VA
Seems straightforward enough, but when I plug in my pressure readings, I'm getting too high of a result for Q (I get a result I'd expect for a fan, and not the dribbling of air I'm actually getting from the pipe).
I think I have the units converted correctly, so am I missing something in the velocity equation?
Here's what I got so far...
I'm assuming laminar, imcompressible flow with negligible friction, head, or thermal losses (this is a very low-flow system). From the Bernoulli equation...
V = (2P/d)^0.5
V = velocity
P = differential pressure
d = air density @ STP
area = A = pi(r^2)
flowrate = Q = VA
Seems straightforward enough, but when I plug in my pressure readings, I'm getting too high of a result for Q (I get a result I'd expect for a fan, and not the dribbling of air I'm actually getting from the pipe).
I think I have the units converted correctly, so am I missing something in the velocity equation?