Shock interaction effect on a flapped delta wing at M equals 8.2
- 1 May 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (5) , 985-986
- https://doi.org/10.2514/3.6322
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Viscous interactions and flight at high Mach numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Effects of shock impingement on the heat transfer around blunt bodies.AIAA Journal, 1968
- A generalization of the direct-stiffness method of structural analysisAIAA Journal, 1964
- NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST THE LOWER SURFACE OF A DELTA WINGAIAA Journal, 1963
- Effect of Wave Interactions on Pressure Distributions in Supersonic and Hypersonic FlowAIAA Journal, 1963