Computations of the Magnus effect for slender bodies in supersonic flow
- 11 August 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Computation of supersonic viscous flows over ogive-cylinders at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Numerical simulation of steady supersonic viscousPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Computations of Magnus effects for a yawed, spinning body of revolutionAIAA Journal, 1978
- Experimental Measurements in the Turbulent Boundary Layer of a Yawed, Spinning Ogive-Cylinder Body of Revolution at Mach 3.0. Part 2. Data TabulationPublished by Defense Technical Information Center (DTIC) ,1978
- 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
- Thin-layer approximation and algebraic model for separated turbulentflowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Viscous flow over a cone at moderate incidence—IComputers & Fluids, 1973