Computation of supersonic laminar viscous flow past a pointed cone at angle of attack in spinning and coning motion
- 10 July 1978
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- 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
- Magnus Forces on Spinning Supersonic Cones -Part I: The Boundary LayerAIAA Journal, 1976
- Calculation of the flow on a cone at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Theoretical analysis of vortex shedding from bodies of revolution inconing motionAIAA Journal, 1971
- Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolutionAIAA Journal, 1970
- Hypothesis for the origin of cross-hatchingAIAA Journal, 1970