Understanding and development of a prediction method of transonic limit cycle oscillation characteristics of fighter aircraft
- 10 August 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Transonic wind tunnel investigation of limit cycle oscillations on fighter type wings - UpdatePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
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