Discontinuous supersonic flow past an ablating wavy wall.
Author:
Affiliation:
1. McDonnell Douglas Astronautics Company, Western Division, Santa Monica, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference5 articles.
1. An Analytic Extension of the Shock-Expansion Method
2. Fig. 1
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1. References;Sedimentary Structures Their Character and Physical Basis Volume II;1982
2. Cross-Hatching Studies-A Critical Review;AIAA Journal;1974-10
3. Three-Dimensional Heat-Transfer and Ablation Disturbances in High-speed Flows;AIAA Journal;1972-12
4. Subsonic and Supersonic Boundary-Layer Flow past a Wavy Wall;AIAA Journal;1972-05
5. Inelastic deformation and crosshatching;AIAA Journal;1971-10
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