Supersonic Laminar Viscous Flow Past a Cone at Angle of Attack in Spinning and Coning Motion
- 1 June 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (6) , 761-768
- https://doi.org/10.2514/3.51132
Abstract
No abstract availableThis publication has 5 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. II - Inviscid flowAIAA 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