A cost-effective method for shock-free supercritical wing design
- 12 January 1981
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- Efficient Transonic Shock-Free Wing Redesign Procedure Using a Fictitious Gas MethodAIAA Journal, 1980
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- Computational transonic design procedure for three-dimensional wings and wing-body combinationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Wing design by numerical optimizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Supercritical Wing Sections IIIPublished by Springer Nature ,1977
- Numerical calculation of transonic flow past a swept wing by a finite volume methodPublished by Office of Scientific and Technical Information (OSTI) ,1977