Shock Wave Boundary-Layer Interactions in Laminar Transonic Flow
- 1 March 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (3) , 323-329
- https://doi.org/10.2514/3.49228
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Shock-wave strength for separation of a laminar boundary layer at transonic speedsAIAA Journal, 1971
- Self-induced separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1969
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- The Theory of Laminar Boundary Layers in Compressible FluidsPhysics Today, 1964
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- REFLECTION AT A LAMINAR BOUNDARY LAYER OF A WEAK STEADY DISTURBANCE TO A SUPERSONIC STREAM, NEGLECTING VISCOSITY AND HEAT CONDUCTIONThe Quarterly Journal of Mechanics and Applied Mathematics, 1950
- Interaction Between Parallel Streams of Subsonic and Supersonic VelocitiesJournal of the Aeronautical Sciences, 1949
- The propagation of steady disturbances in a supersonic stream bounded on one side by a parallel subsonic streamMathematical Proceedings of the Cambridge Philosophical Society, 1948
- The Interaction Between Boundary Layer and Shock Waves in Transonic FlowJournal of the Aeronautical Sciences, 1946