Laminar boundary-layer separation and near-wake flow for a smooth blunt body at supersonic and hypersonic speeds.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (6), 1089-1096
- https://doi.org/10.2514/3.4142
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- 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
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- A study of wakes behind a circular cylinder at m equal 5.7AIAA Journal, 1964
- Near wake of a blunt body at hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- Further solutions of the Falkner-Skan equationMathematical Proceedings of the Cambridge Philosophical Society, 1954