Shock & Detonation Toolbox - Python

• Shock & Detonation Toolbox Python Demos
  • Windows
  • Linux

Rayleigh Line & Hugoniot Curves

• demo_RH.py
  Python 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
Output file: 1, 2, 3, 4