Michiel1984
Aerospace
- Dec 2, 2004
- 14
How do I have to calculate the pressure drop over a restrictor? If I calculate it with the formula stated below, the pressure drop will be huge!!!
Q=Cf*A*SQRT((2*differential pressure)/Density)
A=0.7 mm^2
Q=1.66 GPM
Density=0.997 g/ml
The units have to be calculated in cubic meters and liters (liters/second). The Cf is mostly in between 0.6 and 0.9, but I don't know what the right value of it is. If somebody does know how I can determine the value of it, it would be really great!
Thank you in advance
Ps: the system pressure is 3000 PSI (20,7 MPa)
Q=Cf*A*SQRT((2*differential pressure)/Density)
A=0.7 mm^2
Q=1.66 GPM
Density=0.997 g/ml
The units have to be calculated in cubic meters and liters (liters/second). The Cf is mostly in between 0.6 and 0.9, but I don't know what the right value of it is. If somebody does know how I can determine the value of it, it would be really great!
Thank you in advance
Ps: the system pressure is 3000 PSI (20,7 MPa)