Shock & Detonation Toolbox - Windows

• Shock & Detonation Toolbox Windows Demos

Rayleigh Line & Hugoniot Curves

• 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