Leading-edge vortices and shock-detachment flow over delta wings.
- 1 May 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 6 (3) , 228-232
- https://doi.org/10.2514/3.44040
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- The formulation of a uniform approximation for thin conical wings with sonic leading edgesPublished by Springer Nature ,1964
- An Introduction to the Flow about Plane Swept-back Wings at Transonic SpeedsJournal of the Royal Aeronautical Society, 1960
- Exact and Approximate Solutions for the Supersonic Delta WingJournal of the Aeronautical Sciences, 1956