Unsteady transonic flow calculations for wing-fuselage configurations
- 19 May 1986
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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- A unified approach to the analysis and design of wing-body combinations at subsonic and supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968