wonderlandinirvine
Aerospace
- Apr 9, 2009
- 6
Do anyone recognizes the following Gas Flow formula (for air here)?
W (lbs/sec) = 6.30*Cd* (d^2) *P1 /[(53.34*T)^0.5] * {3.5[(P2/P1)^1.429 - (P2/P1)^1.714]}^0.5
I would appreciate someone can point me to the source.
I understand one from "Crane":
qm' (SCFM) = 678 *Y *(d1^2)* C *{[deltaP*P1'/(T1Sg)]^0.5}
But they have gap and I do not know how to prove they are the same.
Thank you in advance for your kind help.
W (lbs/sec) = 6.30*Cd* (d^2) *P1 /[(53.34*T)^0.5] * {3.5[(P2/P1)^1.429 - (P2/P1)^1.714]}^0.5
I would appreciate someone can point me to the source.
I understand one from "Crane":
qm' (SCFM) = 678 *Y *(d1^2)* C *{[deltaP*P1'/(T1Sg)]^0.5}
But they have gap and I do not know how to prove they are the same.
Thank you in advance for your kind help.