Comparison of high-angle-of-attack slender-body theory and exact solutions for potential flow over an ellipsoid
- 1 June 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 27 (6) , 569-571
- https://doi.org/10.2514/3.25322
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- An improved, robust, axial line singularity method for bodies of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Extension of hypersonic, high-incidence, slender-body similarityAIAA Journal, 1987
- The Pressure Distribution on the Surface of an Ellipsoid in Inviscid FlowAeronautical Quarterly, 1980
- Three-dimensional boundary layer near the plane of symmetry of a spheroid at incidenceJournal of Fluid Mechanics, 1970
- Three-dimensional hypersonic gas flow past slender bodies at high angles of attackJournal of Applied Mathematics and Mechanics, 1960
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949