Slender delta wing at high angles of attack - A flow visualization study
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Self-induced roll oscillations measured on a delta wing/canard configurationJournal of Aircraft, 1986
- Subsonic wing rock of slender delta wingsJournal of Aircraft, 1985
- SupermaneuverabilityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- The fluid mechanics of slender wing rockJournal of Aircraft, 1984
- Dynamic load measurements with delta wings undergoing self-induced roll oscillationsJournal of Aircraft, 1984
- Future fighter technologiesJournal of Aircraft, 1980