Stability and transition on swept wings
- 11 January 1993
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Compressible stability of growing boundary layers using parabolized stability equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Boundary-layer transition - Analysis and prediction revisitedPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Compressible laminar boundary layers with suction on swept and tapered wingsJournal of Aircraft, 1977