Exploratory investigation of the effects of blowing from the leading edge of a delta wing

dc.contributor.author	W. J. G. Trebble	en_US
dc.date.accessioned	2014-10-21T15:56:59Z
dc.date.available	2014-10-21T15:56:59Z
dc.date.issued	1966	en_US
dc.identifier.other	ARC/R&M-3518	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/4095
dc.description.abstract	Low-speed wind-tunnel tests were made to investigate the possibility of increasing the lift of a highly swept wing by ejecting high energy air from the leading edge. The results showed that lift gains were available, but that care should be taken to direct the emergent jet with the minimum possible forward component so that large drag penalties may be avoided.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Exploratory investigation of the effects of blowing from the leading edge of a delta wing	en_US