Numerical application of Evvard's supersonic wing theory to flutter analysis
- 12 May 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Lift Distribution on Supersonic Wings with Subsonic Leading Edges and Arbitrary Angle of Attack DistributionJournal of the Aeronautical Sciences, 1954