Theory of laminar viscous-inviscid interactions in supersonic flow
- 20 January 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
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- Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling.AIAA Journal, 1968
- A second-order weak interaction expansion for moderately hypersonic flow past a flat plate.AIAA Journal, 1967
- Laminar boundary-layer separation and near-wake flow for a smooth blunt body at supersonic and hypersonic speeds.AIAA Journal, 1967
- Mass transfer perturbations about Stewartson's reversed flow profiles.AIAA Journal, 1967
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964
- On the Approximate Solution of the Laminar Boundary-Layer EquationsJournal of the Aeronautical Sciences, 1954
- Further solutions of the Falkner-Skan equationMathematical Proceedings of the Cambridge Philosophical Society, 1954
- On the Boundary-Layer Equations in Hypersonic Flow and Their Approximate SolutionsJournal of the Aeronautical Sciences, 1953