Design of supercritical swept wings
- 1 March 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (3) , 289-291
- https://doi.org/10.2514/3.7912
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Shock-Free Wing DesignAIAA Journal, 1980
- Efficient Transonic Shock-Free Wing Redesign Procedure Using a Fictitious Gas MethodAIAA Journal, 1980
- Technique for developing design tools from the analysis methods of computational aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Numerical calculation of the transonic flow past a swept wing. [FLO 22]Published by Office of Scientific and Technical Information (OSTI) ,1977
- Supercritical Wing Sections IIIPublished by Springer Nature ,1977