Measurements, at mach numbers up to 2.8, of the longitudinal characteristics of one plane and three cambered slender 'ogee' wings

dc.contributor.author	C. R. Taylor	en_US
dc.date.accessioned	2014-10-21T15:55:53Z
dc.date.available	2014-10-21T15:55:53Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/R&M-3328	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3908
dc.description.abstract	Measurements have been made of the longitudinal characteristics of one plane and three cambered slender ogee wings at two subsonic and eight supersonic Mach numbers up to 2.8. The tests also included measurements of the zero-lift pressure drag and support interference of the plane wing. The results have been analysed to give data for estimating the performance of supersonic transport aircraft.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Measurements, at mach numbers up to 2.8, of the longitudinal characteristics of one plane and three cambered slender 'ogee' wings	en_US