Glenn
Research
Center
R = Gas Constant y =Specitic Fleat Ratio
7*1
2(7-1)
A=Area r s Density V=Velocity M = Mach T= Temperaturę p=Pressure t denotes total conditions
Mass Flow Ratę:
m = r V A
For an ideał compressible gas:
m
At the throat, the area is a minimum and M—i.O.
For M = 1.0 m = .532 AjJt_ |bs/sec A in ft* p in pst, (Air) -/Tt T in Rankine