Viscous Flow over Spinning Cones at Angle of Attack
- 1 July 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (7) , 975-985
- https://doi.org/10.2514/3.49389
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- A Magnus theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Viscous flow over a cone at moderate incidence—IComputers & Fluids, 1973
- A numerical method for three-dimensional viscous flow: Application to the hypersonic leading edgeJournal of Computational Physics, 1972
- Navier-Stokes solutions for laminar incompressible flow over yawed spinning bodies of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Hypersonic boundary layer studies on a spinning sharp cone at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Hypersonic interactions near sharp leading edges.AIAA Journal, 1969
- Magnus characteristics of finned and nonfinned projectilesAIAA Journal, 1965
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949