A theoretical investigation for delta wings with leading-edge separation at low speeds

dc.contributor.author	R. K. Nangia	en_US
dc.contributor.author	G. J. Hancock	en_US
dc.date.accessioned	2014-10-20T11:05:36Z
dc.date.available	2014-10-20T11:05:36Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-1086	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1099
dc.description.abstract	A non-linear lifting surface theory is postulated which incorporates the leading edge separations, by extending Brown and Michael's slender wing model, but satisfies the Kutta trailing edge condition. Results of a numerical application to a delta wing indicate acceptable trends compared with experimental data.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	A theoretical investigation for delta wings with leading-edge separation at low speeds	en_US