The theoretical relationships for an aerofoil with a multiply hinged flap system

dc.contributor.author	W. G. A. Perring
dc.date.accessioned	2014-10-21T12:03:36Z
dc.date.available	2014-10-21T12:03:36Z
dc.date.issued	1928
dc.identifier.other	ARC/R&M-1171	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1467
dc.description.abstract	Theoretical expressions for the lift and pitching moment of an aerofoil in two dimensional motion were developed in R&M 910. This theory was extended in R&M 1095 to include the hinge moment of a flap in the case of a rectangular aerofoil of finite span. This analysis has now been extended to an aerofoil fitted with a multiply hinged flap system, and theoretical expressions for lift and pitching moment of the aerofoil, and the hinge moment about any hinge position have been deduced in the case of a rectangular aerofoil of finite span.	en_US
dc.language.iso	en	en_US
dc.publisher	H. M. Stationery Office	en_US
dc.relation.ispartofseries	Aeronautical Research Committee Reports & Memoranda	en_US
dc.title	The theoretical relationships for an aerofoil with a multiply hinged flap system	en_US
dc.type	Technical Report	en_US