Isothermal gas flow

Molecular weight of gas, M_w = .

Pipe area, A = 0.0000e+0 ft2 .

Pressure at condition 1, P1 = 0.0000e+0 lb per ft2 .

Density at condition 1, rho1 = 0.0000e+0 lb per ft3 .

Mass velocity, G1 = 0.0000e+0 lb per ft2 per sec .

Speed of sound at condition 1, c1 = 0.0000e+0 ft per sec .

Mach number at condition 1, M1 = 0.0000e+0 .

Pressure at condition 2, P2 = 0.0000e+0 lb per ft2.

Density at condition 2, rho2 = 0.0000e+0 lb per ft3 .

Velocity at condition 2, V2 = 0.0000e+0 ft per sec .

Mach number at condition 2, M2 = 0.0000e+0 .

Pressure drop, delta_p = 0.0000e+0 lb per ft2.

Heat transferred, q_h = 0.0000e+0 Btu per lb.


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Isothermal gas flow

For a gas that flows through a pipe, under isothermal conditions, find out the necessary information.
T1 (Temperature, deg F)
P1 (Pressure at condition 1, psi)
P2 (Pressure at condition 2, psi)
w (Mass flow rate, lb per sec)
k (Ratio of cp to cv)
M_w (Mol wt of gas)
f (friction factor)
d (Pipe diameter, inch)
L (Pipe length, ft)
V1 (Velocity, ft per sec)
V2 (Velocity, ft per sec)
delta_p (Pressure Drop, lbf per in2)
Missing Valuepressure drop length