The Longitudinal Characteristics of Three Slender "Mild Ogee" Wings at Mach Numbers from 0.4 to 2.0

dc.contributor.author	D.G. Mabey	en_US
dc.contributor.author	G.P. Ilott	en_US
dc.date.accessioned	2014-10-20T11:05:05Z
dc.date.available	2014-10-20T11:05:05Z
dc.date.issued	1967	en_US
dc.identifier.other	ARC/CP-1006	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1019
dc.description.abstract	Wind tunnel measurements of lift, pitching moment and drag on one plane and two cambered wings of "mild ogee" planfom (p = 8/15) are reported. These measurements are supplemented by vapour screen and oil flow observations. The wings were designed by slender wing theory for attached flow along the leading-edge at particular values of lift and pitching moment. The design and measured attachment conditions agreed fairly well. The non-linear lift developed could be related with the type of vortex development above the attachment incidence.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The Longitudinal Characteristics of Three Slender "Mild Ogee" Wings at Mach Numbers from 0.4 to 2.0	en_US