Theoretical studies to refine the prediction of unsteady aerodynamics of supersonic elastic aircraft
- 16 August 1970
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- FURTHER DEVELOPMENTS IN SUPERSONIC AERODYNAMIC INFLUENCE COEFFICIENT METHODSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic EdgesJournal of the Aeronautical Sciences, 1955