Low-speed wind-tunnel tests on a model of a jet tailles aircraft

dc.contributor.author	J. Trouncer	en_US
dc.contributor.author	G. F. Moss	en_US
dc.date.accessioned	2014-10-21T15:53:11Z
dc.date.available	2014-10-21T15:53:11Z
dc.date.issued	1947	en_US
dc.identifier.other	ARC/R&M-2843	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3400
dc.description.abstract	This report gives the results of longitudinal and lateral stability tests made on a model of a jet tailless aircraft. It includes the effects of split flaps, trimming flaps, dive-recovery flaps and four types of anti-tip-stalling device (slats, nose flaps, double split flaps and letter-box slots). It also includes the effect of the ground in the landing condition.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Low-speed wind-tunnel tests on a model of a jet tailles aircraft	en_US