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The Solution of Aeroelastic Problems on Wings of Arbitrary Plan Form by Matrix Methods

Published online by Cambridge University Press:  28 July 2016

J. J. Foody  and
L. Reid
J. J. Foody
Affiliation:
Short Brothers and Harland Ltd.
L. Reid
Affiliation:
Short Brothers and Harland Ltd.
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Summary

It has been adequately demonstrated that the reduction of structural and aeroelastic problems to a form suitable for computation is best done using a matrix formulation. The present paper outlines such a formulation of the aeroelastic problems on wings of arbitrary plan form and gives a method of solution which has been found satisfactory over a wide range of practical calculation. In the symmetric case the problem of manoeuvre margin due to aeroelastic effect is considered and in the anti-symmetric case the rolling effectiveness and the reversal speed for aileron controls are dealt with.

Type
Research Article
Information
The Aeronautical Journal , Volume 59 , Issue 540 , December 1955 , pp. 843 - 846
Copyright
Copyright © Royal Aeronautical Society 1955

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References

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4. Short Brothers and Harland Ltd. The Inversion of Matrices by Triangular Resolution. Aero. Report No. 69.Google Scholar
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