Shock & Detonation Toolbox - Python


Rayleigh Line & Hugoniot Curves



Input Data
Mixture Stoichiometric H2/Air
'H2:2 O2:1 N2:3.76'
Mechanism h2air_highT.cti
Initial Pressure 1 bar = 100000 Pa
Initial Temperature 300 K
Overdrive for Rayleigh Line 1.0
Gamma (Ratio of Specific Heats) 1.4
Output Data
Output file: 1, 2, 3, 4