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 equilibrium.
Test is 'experiment'
Facility is x2.
Driver gas is {'Ar': 0.2, 'He': 0.8} (by moles).
Test gas (state 1) is gasgiant_h285ne (gamma = 1.6078, R = 476.310512747, {'H2': 0.15, 'Ne': 0.85} by moles).
Accelerator gas (state 5) is Air.
Vs1 = 3057.74 m/s, Ms1 = 6.40, Vs2 = 6720.43 m/s, Ms2 = 19.42
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  10.46800 15500.0 15.500   
s3s   7.551e+06  1495.3   1361  1359.7   1.00  6.79690  15500.0 15.471   
s1    2000.0     298.1    478   0.0      0.00  0.01408  2.0     0.002    
s2    107510.0   3080.3   1377  2450.3   1.78  0.07089  457.6   0.568    
s3    1.592e+06  802.6    997   2450.3   2.46  2.67010  14859.4 25.078   
s5    1.0        298.1    346   0.0      0.00  1.17e-05 0.0     0.000    
s6    499.0295   5301.3   1633  6342.5   3.88  2.08e-04 8.4     0.172    
s7    125.9287   322.7    497   6720.4   13.52 8.19e-04 33.0    22.623   
s8    7.585137   110.3    292   6759.8   23.11 1.44e-04 5.9     22.591   
s10f  5018.354   17557.7  3691  5133.2   1.39  6.00e-04 13.7    0.010    
s10e  5619.0     10132.5  2665  5748.8   2.16  9.65e-04 33.2    0.056    
s10cf 489.6711   1714.8   1153  6464.5   5.60  6.00e-04 22.4    0.237    
s10c  488.5144   1650.2   1102  6466.8   5.87  6.21e-04 23.5    1.720    
The total enthalpy (Ht) leaving the nozzle is 22.613 MJ/kg (H8 - h1).
The total temperature (Tt) leaving the nozzle is 13441 K.
The freestream enthalpy (h) leaving the nozzle is -0.2343 MJ/kg (h8 - h1).
The flight equivalent velocity (Ue) is 6725 m/s.
Basic test time = 61.40 microseconds
Species in the shock layer at equilibrium (s10e) (by moles):
{'e-': 0.046354, 'H': 0.20263, 'Ne+': 0.00020291, 'Ne': 0.70467, 'H+': 0.046151}