Viscous Interaction Theory for Slender Axisymmetric Bodies in Hypersonic Flow
Author:
Affiliation:
1. The Aerospace Corporation, El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55430
Reference15 articles.
1. Hayes, W. D. and Probstein, R. F., Hypersonic Flow Theory, Academic, New York, 1959,pp.333-370.
2. The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer Flow
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