A nonasymptotic triple deck model for supersonic boundary-layer interaction
Author:
Affiliation:
1. The City College of The City University of New York, New York
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
1. 'Lighthill, M.J. "On Boundary-Layers and Upstream Influence, II. Supersonic Flows without Separation,"A,217, 1953; pp.478-507.
2. Self-induced separation
3. On self‐induced separation II
4. Base pressure in laminar supersonic flow
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1. Application of the triple-deck theory of viscous-in viscid interaction to bodies of revolution;Journal of Fluid Mechanics;1983-04
2. D’Alembert’s Paradox;SIAM Review;1981-07
3. UPSTREAM INFLUENCE AND SKIN FRICTION IN NON-SEPARATING SHOCK-TURBULENT BOUNDARY LAYER INTERACTIONS;13th Fluid and PlasmaDynamics Conference;1980-07-14
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