A theory of the flow past a slender delta wing with leading edge separation
- 26 May 1959
- journal article
- Published by The Royal Society in Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences
- Vol. 251 (1265) , 200-217
- https://doi.org/10.1098/rspa.1959.0102
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Effect of Leading-Edge Separation on the Lift of a Delta WingJournal of the Aeronautical Sciences, 1954
- Leading-Edge Separation from Delta Wings at Supersonic SpeedsJournal of the Aeronautical Sciences, 1953
- Ausbildung eines Wirbels an der Kante einer PlatteArchive of Applied Mechanics, 1939
- Aufwicklung einer unstabilen UnstetigkeitsflächeArchive of Applied Mechanics, 1931