Chemical and vibrational relaxation of an inviscid hypersonic flow
Author:
Affiliation:
1. Avco Corporation, Wilmington, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2659
Reference27 articles.
1. On the calculation of flow past axisymmetric bodies with detached shock waves using an electronic computing machine
2. G. The Method of Characteristics
3. A STREAMTUBE APPROXIMATION FOR CALCULATION OF REACTION RATES IN THE INVISCID FLOW FIELD OF HYPERSONIC OBJECTS
4. Inviscid Flow with Nonequilibrium Molecular Dissociation for Pressure Distributions Encountered in Hypersonic Flight
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