Multizone Euler marching technique for flow over single and multibody configurations
Author:
Affiliation:
1. Rockwell International Science Center, Thousand Oaks, CA
2. Rockwell International Corp., Space Div., Downey, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-592
Reference7 articles.
1. Euler solver for three-dimensional supersonic flows with subsonic pockets
2. Approximate Riemann solvers, parameter vectors, and difference schemes
3. Chakravarthy, S.R. and Ota, D. "Numerical Issues in Computing Inviscid Supersonic Flow Over Conical Delta Wings;' AIAA Paper Nc. 86-0440, Jan. 1986.
4. SVCDS - An evolutionary CDS for preliminary space vehicle design, analysis, and simulation
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