calzone
Aerospace
- May 24, 2016
- 1
I'm working on a valve sizing problem and have encountered some valve equations and measurements that I do not understand.
In Flow Equations for Sizing Control Valves ISA-75.01.01-2007 (pdf), equation 14b (Page 17) provides the flow coefficient for turbulent, choked flow to be: C = Q/(0.667N7P1)*SQRT[(GgT1Z)/(FyXT)]
The term of interest is xT, which is the critical pressure drop ratio at which the valve is choked. xT = (P0 - P)/P0
I understand that for air, the critical ratio across an orifice is P/P0 = 0.53, which corresponds to an xT of 0.47. However, the document linked above (Table 2, page 26) provides some example measurements for valves and shows xT to vary from 0.2 to 0.84 (suggesting critical pressure ratios P/P0 of 0.8 to 0.14).
I can understand how internal frictional losses might reduce the critical pressure ratio (thus increasing xT), but I cannot find a reason why the critical pressure ratio could be any higher than 0.53 (xT would be any lower than 0.47).
Can someone help me understand these critical pressure ratios in valves?
In Flow Equations for Sizing Control Valves ISA-75.01.01-2007 (pdf), equation 14b (Page 17) provides the flow coefficient for turbulent, choked flow to be: C = Q/(0.667N7P1)*SQRT[(GgT1Z)/(FyXT)]
The term of interest is xT, which is the critical pressure drop ratio at which the valve is choked. xT = (P0 - P)/P0
I understand that for air, the critical ratio across an orifice is P/P0 = 0.53, which corresponds to an xT of 0.47. However, the document linked above (Table 2, page 26) provides some example measurements for valves and shows xT to vary from 0.2 to 0.84 (suggesting critical pressure ratios P/P0 of 0.8 to 0.14).
I can understand how internal frictional losses might reduce the critical pressure ratio (thus increasing xT), but I cannot find a reason why the critical pressure ratio could be any higher than 0.53 (xT would be any lower than 0.47).
Can someone help me understand these critical pressure ratios in valves?