Vortex sheets rolling-up along leading-edges of delta wings
- 31 December 1966
- journal article
- Published by Elsevier in Progress in Aerospace Sciences
- Vol. 7, 7-33
- https://doi.org/10.1016/0376-0421(66)90004-2
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Possible Types of Flow at Swept Leading EdgesAeronautical Quarterly, 1964
- Nichtlineare Tragflächentheorie insbesondere für Tragflügel mit kleinem SeitenverhältnisArchive of Applied Mechanics, 1961
- A theory of the flow past a slender delta wing with leading edge separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1959
- Remarques sur l'écoulement tourbillonnaire autour des ailes en flècheZeitschrift für angewandte Mathematik und Physik, 1958
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949