Numerical Computation of Hypersonic Viscous Flow over a Sharp Leading Edge
- 1 February 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (2) , 129-130
- https://doi.org/10.2514/3.49181
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Leading edge flow by the Monte Carlo direct simulation techniqueAIAA Journal, 1970
- Numerical Solutions of Hypersonic Sharp-Leading-Edge FlowsPhysics of Fluids, 1967