Sweepback Effects in Turbulent Boundary-Layer Shock-Wave Interaction
- 1 May 1960
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (5) , 348-356
- https://doi.org/10.2514/8.8538
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Discussion: “Theory for Base Pressures in Transonic and Supersonic Flow” (Korst, H. H., 1956, ASME J. Appl. Mech., 23, pp. 593–600)Journal of Applied Mechanics, 1957
- Separation of a Supersonic Turbulent Boundary LayerJournal of the Aeronautical Sciences, 1955
- 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