Calculation of supersonic flows with strong viscous-inviscid interaction
Author:
Affiliation:
1. University of Cincinnati, Cincinnati, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9552
Reference16 articles.
1. Hypersonic viscous flow over slender bodies with sharp leading edges.
2. Numerical solution of the hypersonic viscous shock-layer equations
3. Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
4. A Review of Marching Procedures for Parabolized Navier-Stokes Equations
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