Aeroelastic Criterion for Leading Edge Stiffness

M.J. Wooldridge, B.Sc. (Research Technician, Future Projects Group, Sir W. G. Armstrong Whitworth Aircraft Ltd.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 July 1960

Abstract

A composite chart is presented to facilitate the rapid determination of a critical divergence stiffness for a straight or swept leading edge of a lifting surface. The aeroelastic criterion is intended for use in initial design work and there is scope for the inclusion of other materials than those shown. To accommodate the effects of kinetic heating the material temperature has been taken identical to that of the boundary layer adjacent to it.

Citation

Wooldridge, M. (1960), "Aeroelastic Criterion for Leading Edge Stiffness", Aircraft Engineering and Aerospace Technology, Vol. 32 No. 7, pp. 192-194. https://doi.org/10.1108/eb033272

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Publisher

:

MCB UP Ltd

Copyright © 1960, MCB UP Limited

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