Table of Flow Properties -- For a Shock Tube

Input flow variable:

gamma1:

R1:

P1:

T1(in K):

gamma4:

R4:

P4:

T4(in K):

Initial guess P2/P1(>=1):
Tolerance:
Number of iterations:
Elapsed time(sec):

Output Flow Properties:

1. Velocities (m/s)
front wavetail wavecontact surfaceshock wave

2. Distances (m) of (w.r.t. diaphragm location)
front wavetail wavecontact surfaceshock wave

3. Temperatures of T2 and T3 ; Shock Mach No. (MS)
T2T3MS

4. Properties in the expansion waves
LocationSonicVelocityPressureTemperature DensityMach No.

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