Interacting supersonic laminar wake calculations by a finite difference method.
Author:
Affiliation:
1. TRW Systems, Redondo Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4175
Reference8 articles.
1. A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic Streams
2. Lees, L. and Reeves, B. L. "Supersonic separated and reattaching laminar flows: I. general theory and application to adiabatic boundary layer-shock wave interactions/' AIAA J. 2,629-636(1964).
3. Theory of laminar near wake of blunt bodies in hypersonic flow.
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