Free flight measurements of the longitudinal stability of a transonic swept-winged aircraft

dc.contributor.author	G. K. Hunt	en_US
dc.date.accessioned	2014-10-20T11:05:30Z
dc.date.available	2014-10-20T11:05:30Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-1052	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1065
dc.description.abstract	Four models of an aircraft configuration with a 55 degree swept wing were flown at Mach numbers between 0.9 end 1.4, at Reynolds numbers up to 10 million and lift coefficients between zero and 0.5. Measurements of the manoeuvre margin and the derivatives ... were obtained. The results are compared with those obtained from one of the same models in a transonic wind tunnel and from a related M-wing model in flight. They are also corrected for aeroelastic effects.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Free flight measurements of the longitudinal stability of a transonic swept-winged aircraft	en_US