Hypersonic boundary-layer separation and the base flow problem.
- 1 August 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (8) , 1321-1330
- https://doi.org/10.2514/3.3672
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Rapid expansion of a supersonic boundary layer and its application to the near wake.AIAA Journal, 1966
- Near wake flow field measurements.AIAA Journal, 1965
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- Near wake of a blunt body at hypersonic speedsAIAA Journal, 1965
- Recent Studies of the Laminar Base-Flow RegionAIAA Journal, 1964
- Momentum integral methods for the laminar free shear layerAIAA Journal, 1964
- COMPRESSIBLE FREE SHEAR LAYER WITH FINITE INITIAL THICKNESSAIAA Journal, 1963
- Some remarks on the flat plate boundary layerQuarterly of Applied Mathematics, 1949
- On the propagation of small disturbances in a moving compressible fluidQuarterly of Applied Mathematics, 1946