Effects of gas models on hypersonic base flow calculations
Author:
Affiliation:
1. University of Illinois, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26426
Reference5 articles.
1. 2Park, C. "Assessment of Two-Temperature Kinetic Model for Ionizing Air,"AIAA Paper 87-1574, June 1987.
2. Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
3. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
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