Lift Distribution on Supersonic Wings with Subsonic Leading Edges and Arbitrary Angle of Attack Distribution
- 1 November 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (11) , 783-785
- https://doi.org/10.2514/8.3208
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Energy Approach to the General Aircraft Performance ProblemJournal of the Aeronautical Sciences, 1954
- The lift of a delta wing at supersonic speedsQuarterly of Applied Mathematics, 1946