A Cost-Effective Method for Shock-Free Supercritical Wing Design
- 1 April 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (4) , 283-289
- https://doi.org/10.2514/3.57391
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- THE AERODYNAMIC DESIGN OF SECTION SHAPES FOR SWEPT WINGSPublished by Elsevier ,1962