Wing-body carryover at supersonic speeds with finite afterbodies
- 1 May 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (5) , 661-664
- https://doi.org/10.2514/3.7807
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
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- Test Time and Particle Paths in Low-Pressure Shock TubesPhysics of Fluids, 1966
- Flow Nonuniformity in Shock Tubes Operating at Maximum Test TimesPhysics of Fluids, 1966
- On Flow Duration in Low-Pressure Shock TubesPhysics of Fluids, 1960