Computational Transonic Optimization and Wind-Tunnel Test of a Semispan Wing
- 1 September 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (9) , 606-610
- https://doi.org/10.2514/3.58414
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Relaxation methods for transonic flow about wing-cylinder combinations and lifting swept wingsPublished by Springer Nature ,2007
- Numerical calculation of transonic flow about swept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Analysis and design of wing-body combinations at subsonic and supersonic speeds.Journal of Aircraft, 1968