A Theoretical Model of the Near Wake of a Slender Body in Supersonic Flow
Author:
Affiliation:
1. TRW Systems Group, Redondo Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50344
Reference23 articles.
1. An interaction model of a supersonic laminar boundary layer on sharpand rounded backward facing steps.
2. Upstream Influence in Viscous Interaction Problems
3. A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic Streams
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