Computation of hypersonic viscous flow over a body with mass transfer and/or spin
- 1 March 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 20 (2) , 101-107
- https://doi.org/10.2514/3.28364
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt BodiesAIAA Journal, 1978
- Computation of supersonic laminar viscous flow past a pointed cone at angle of attack in spinning and coning motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Heat- and mass-transfer effects on three-dimensional hypersonic viscous shock-layer flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Computation of hypersonic laminar viscous flow past spinning sharp and blunt cones at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Hypersonic viscous flows over sphere-cones at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Calculation of the Flow on a Cone at High Angle of AttackAIAA Journal, 1974
- NUMERICAL SOLUTIONS TO THE VISCOUS SHOCK-LAYER BLUNT BODY PROBLEM WITH INERT GAS INJECTION.Published by Office of Scientific and Technical Information (OSTI) ,1971