Theory of laminar viscous-inviscid interactions in supersonic flow
- 1 December 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (12), 2211-2221
- https://doi.org/10.2514/3.5518
Abstract
No abstract availableThis publication has 15 references indexed in Scilit:
- Theory of laminar viscous-inviscid interactions in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Upstream Influence in Viscous Interaction ProblemsPhysics of Fluids, 1968
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA 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
- Correlated incompressible and compressible boundary layersProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1949
- Approximate Calculation of the Laminar Boundary LayerAeronautical Quarterly, 1949
- Anwendung des Energiesatzes von Wieghardt auf einparametrige Geschwindigkeitsprofile in laminaren GrenzschichtenArchive of Applied Mechanics, 1948
- CVI.An approximate solution of the boundary layer equations for a flat plateJournal of Computers in Education, 1937