Computation of hypersonic laminar viscous flow past spinning sharp and blunt cones at high angle of attack
- 16 January 1978
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Magnus forces on spinning supersonic cones. II - Inviscid flowAIAA Journal, 1976
- Boundary-Layer Separation in Unsteady FlowSIAM Journal on Applied Mathematics, 1975
- Viscous Flow over Spinning Cones at Angle of AttackAIAA Journal, 1974
- Calculation of the flow on a cone at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Laminar Boundary Layer on a Spinning Cone at Small Angles of Attack in a Supersonic FlowJournal of the Aeronautical Sciences, 1957