- demo_RH.m

Matlab program used to generate the sample output described below

- Numerical Solution Methods for Shock and Detonation Jump Conditions

Documentation discussing algorithm used for this demo

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 |