Browsing Aeronautical Research Committee Reports & Memoranda by Author "A. S. Batson"

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Effect on hinge moment of fitting strips near aileron trailing edge, of increasing aileron chord and of extending aileron to wing tip with an appendix on pressures over surface of control fitted with strips

A. S. Batson; J. H. Warsap (H. M. Stationery Office, 1940)

To find a method Of modifying ailerons so that a machine may be more responsive in roll. (1) Hinge moment was measured on a 1/2.25 scale 'Hurricane' aileron with the following modifications:- (a) Strips (depth 0.02 in. and ...

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