Magnus Forces on Spinning Supersonic Cones -Part I: The Boundary Layer
- 1 April 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (4) , 498-504
- https://doi.org/10.2514/3.61389
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Viscous Flow over Spinning Cones at 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
- A Magnus theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,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
- Boundary layer on a hypersonic sharp cone at small angle of attackAIAA Journal, 1971
- Comment on "Solution of a Three-Dimensional Boundary-Layer Flow with Separation"AIAA Journal, 1969
- Solution of a three-dimensional boundary-layer flow with separation.AIAA Journal, 1968