Shock & Detonation Toolbox - Windows


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
CJ speed 1967.8451 m/s
Output file: 1, 2, 3, 4




Rayleigh Line with CJ speed slope
Reactant & Product Hugoniots
Identical plot as left, but with additional lower bound
discussed in
Numerical Solution Methods for Shock and Detonation Jump Conditions