Magnus forces on spinning supersonic cones. I - The boundary layer
- 20 January 1975
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Calculation of the Flow on a Cone at High Angle of AttackAIAA Journal, 1974
- Laminar boundary layer over a body of revolution at extremely high incidencePhysics of Fluids, 1974
- Calculation of Unsteady and Three-Dimensional Boundary-Layer FlowsAIAA Journal, 1973
- Boundary layer studies on a spinning conePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Crossflow and Unsteady Boundary-Layer Effects on Rotating BladesAIAA Journal, 1971
- Solution of a three-dimensional boundary-layer flow with separation.AIAA Journal, 1968