jobarrco
Mechanical
- Jun 8, 2012
- 5
Hello,
I'm not a fluids guy... but I need to determe the pressure drop of a natural gas supply line.
The line size is fixed - 2 inches. I'm trying to flow 47,100 ft^3/hr (1,2627 lb/hr) with an inlet pressure of 94.7 psia.
After a few calcs the mach number at the inlet is .411.
I'm a little lost on the theory now. I used the Fanno flow equations and determined the flow is choked.
L* = 2.77 ft <<< Normal shock at 2.77 ft?
P* = 60.4 psia
V* = 1378 ft/sec <<< the initial velocity increased to 1378 ft/sec? but constant mass flow rate = change in density?
So now I know the conditions at L*... how do I determine the conditions at L = 150 ft?
I have the Crane TP410 - I'm not sure it is useful for this problem though.
If anyone can recommend any other books, that would be helpful too.
I searched the forum and found a reference to another thread that describes compressible flow, but had no luck finding it.
Thank you!
I'm not a fluids guy... but I need to determe the pressure drop of a natural gas supply line.
The line size is fixed - 2 inches. I'm trying to flow 47,100 ft^3/hr (1,2627 lb/hr) with an inlet pressure of 94.7 psia.
After a few calcs the mach number at the inlet is .411.
I'm a little lost on the theory now. I used the Fanno flow equations and determined the flow is choked.
L* = 2.77 ft <<< Normal shock at 2.77 ft?
P* = 60.4 psia
V* = 1378 ft/sec <<< the initial velocity increased to 1378 ft/sec? but constant mass flow rate = change in density?
So now I know the conditions at L*... how do I determine the conditions at L = 150 ft?
I have the Crane TP410 - I'm not sure it is useful for this problem though.
If anyone can recommend any other books, that would be helpful too.
I searched the forum and found a reference to another thread that describes compressible flow, but had no luck finding it.
Thank you!