Transonic wind tunnel investigation of limit cycle oscillations on fighter type wings - Update
- 16 April 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Understanding and development of a prediction method of transonic limit cycle oscillation characteristics of fighter aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Low-Speed Unsteady Aerodynamics of a Pitching Straked Wing at High Incidence-Part I: Test ProgramJournal of Aircraft, 1990
- Transonic Flow about a Thick Circular-Arc AirfoilAIAA Journal, 1976