Boundary-layer displacement and leading edge bluntness effects on attached and separated laminar boundary layers in a compression corner.I - Theoretical study
- 22 January 1968
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Optimization of a lateral turn at constant height.AIAA Journal, 1967
- BIRDS OF MAURITIUS AND REUNIONOstrich, 1966
- Modified Crocco-Lees Mixing Theory for Supersonic Separated and Reattaching FlowsJournal of the Aerospace Sciences, 1962
- On the Approximate Solution of the Laminar Boundary-Layer EquationsJournal of the Aeronautical Sciences, 1954
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952