Thesis/data/misc/x2s4111/databox/x2s4111pg_theoretical.txt
2024-10-17 19:30:54 +10:00

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Pitot Version: 15-Aug-2018 doing an expansion tube calculation
state 4 is the driver condition.
state 1 is shock tube fill. state 5 is acceleration tube fill.
state 2 is the shocked test gas.
state 7 is expanded test gas entering the nozzle.
state 8 is test gas exiting the nozzle (using area ratio of 5.64).
state 10f is frozen shocked test gas flowing over the model.
state 10e is equilibrium shocked test gas flowing over the model.
state 10c is conditions over 15.0 degree conehead in the test section.
Solver used is perfect gas.
Test is 'fulltheory-pressure'
Facility is x2.
Driver gas is He:0.80,Ar:0.20.
Test gas (state 1) is gasgiant_h285ne (gamma = 1.6078, R = 476.310512747).
Accelerator gas (state 5) is Air.
Vs1 = 4521.09 m/s, Ms1 = 9.46, Vs2 = 10323.69 m/s, Ms2 = 29.83
state P T a V M rho pitot stgn
Pa K m/s m/s kg/m^3 kPa MPa
s4 1.550e+07 1993.0 1571 0.0 0.00 10.46941 15500.0 15.500
s3s 7.551e+06 1494.7 1360 1360.4 1.00 6.80010 15500.0 15.500
s1 2000.0 298.1 478 0.0 0.00 0.01408 2.0 0.002
s2 220307.2 7935.9 2465 3428.6 1.39 0.05828 721.4 0.748
s3 216358.6 360.9 668 3428.6 5.13 0.80696 8456.5 64.527
s5 1.0 298.1 346 0.0 0.00 1.17e-05 0.0 0.000
s6 1037.642 51852.0 4565 8593.4 1.88 6.97e-05 5.2 0.007
s7 12.92844 199.5 391 10227.2 26.16 1.36e-04 12.7 17.751
s8 0.7990541 69.7 231 10243.1 44.35 2.41e-05 2.2 17.750
s10f 1937.917 39436.9 5496 7851.8 1.43 1.03e-04 6.6 0.007
s10e 2287.0 12973.2 3227 9268.3 2.87 2.53e-04 22.1 0.093
s10c 184.495 3615.9 1664 9802.9 5.89 1.07e-04 9.2 0.119
The total enthalpy (Ht) leaving the nozzle is 52.172 MJ/kg (H8 - h1).
The total temperature (Tt) leaving the nozzle is 41705 K.
The freestream enthalpy (h) leaving the nozzle is -0.2879 MJ/kg (h8 - h1).
The flight equivalent velocity (Ue) is 10215 m/s.
Basic test time = 20.08 microseconds
Species in the shock layer at equilibrium (s10e) (by moles):
{'e-': 0.21377, 'H': 0.026268, 'Ne+': 0.03494, 'Ne': 0.54618, 'H+': 0.17883}