Experiments giving hinge moment and lift on a NACA 0015 aerofoil fitted with a 40 per cent control, with especial reference to effect of curvature of control surface

dc.contributor.author	A. S. Batson	en_US
dc.contributor.author	J. H. Preston	en_US
dc.contributor.author	J. H. Warsap	en_US
dc.date.accessioned	2014-10-21T15:52:23Z
dc.date.available	2014-10-21T15:52:23Z
dc.date.issued	1943	en_US
dc.identifier.other	ARC/R&M-2698	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3243
dc.description.abstract	To add to the available data regarding lift and hinge moment on a control, and to test further the ideas developed in R. & M. 20O8, with especial reference to the effect of curvature of control surface. Measurement of lift and hinge moment on a two-dimensional aerofoil (section NACA 0015, chord 18 in.) fitted with a 40 per cent control (radius-nose).	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Experiments giving hinge moment and lift on a NACA 0015 aerofoil fitted with a 40 per cent control, with especial reference to effect of curvature of control surface	en_US