Effects of flap length and slot suction on separated laminar boundary layers
- 20 January 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An investigation of the effect of suction on hypersonic laminar boundary-layer separation.AIAA Journal, 1968
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964