Recent Developments in the Structural Approach to Aeroelastic Problems

Author:

Williams D.

Abstract

The 899th Lecture to be given before the Royal Aeronautical Society was held on 11th February 1954 at the Institution of Mechanical Engineers, Storey's Gate, London, S.W.I. Mr. G. R. Edwards, C.B.E., F.R.Ae.S., Vice-President of the Society, presided. Introducing the Lecturer, Dr. D. Williams, M.I.Mech.E., F.R.Ae.S., Mr. Edwards said that Dr. Williams was really too well known to need any introduction; his activities had been devoted in recent years to structural problems as applied to aeroplanes. Without reciting his attainments in detail, the job he had tackled in recent years at the Royal Aircraft Establishment and about which he had written papers, covered such subjects as vibration, wing flutter, sandwich construction, the effect of blast on aeroplanes, energy theorems, fatigue, dynamic loading by gusts and landing impacts, water-borne runways and nose-wheel shimmy, a variety of subjects one or all of which had caused most of them a great deal of anguish at one time or another.

Publisher

Cambridge University Press (CUP)

Reference11 articles.

1. Hall A. H. (1953). A Simplified Theory of Swept Wing Deformation. N.A.E.C. Report No. 19, 1953.

2. Structural Analysis and Influence Coefficients for Delta Wings;Levy;Journal of the Aeronautical Sciences,1953

3. Stein M. and Anderson J. E. (1952). Deflection and Stress Analysis of Thin Solid Wings of Arbitrary Plan Form with particular reference to Welta Wings. N.A.C.A. T.N. 2621, February 1952.

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2. Use of Modern Computers in Structural Analysis;Journal of the Structural Division;1958-05

3. Solution of Aeroelastic Problems by Means of Influence Coefficients;The Journal of the Royal Aeronautical Society;1957-04

4. The Vibration of Frames;Proceedings of the Institution of Mechanical Engineers;1956-06

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