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The Deformational Behaviour of Low Aspect Ratio Multi-Web Wings*

PART II: Elementary and Plate Bending Theories

Published online by Cambridge University Press:  07 June 2016

R. H. Gallagher  and
I. Rattinger
R. H. Gallagher
Affiliation:
Aerospace Department, Bell Aerosystems Company
I. Rattinger
Affiliation:
Aerospace Corporation
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Summary

Results of a study of the accuracy attainable from various approaches to low aspect ratio wing deformational analyses are described. Seven model multi-web wings, representing a restricted range of sweep angles, aspect ratios and other geometric factors, were tested for deflection influence coefficients; Part I gave experimental data. This paper describes, applies, and compares certain elementary and plate bending theories. A subsequent paper will deal with discrete element idealisations commonly employed in matrix structural analysis.

Information

Type
Research Article
Information
Aeronautical Quarterly , Volume 13 , Issue 1 , February 1962 , pp. 71 - 87
Copyright
Copyright © Royal Aeronautical Society. 1962

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References

2. Gallagher, R. H. and Rattinger, I. The Deformational Behaviour of Low Aspect Ratio Multi-Web Wings, Part I: Experimental Data. Aeronautical Quarterly, Vol. XII, p. 361, November 1961.Google Scholar
3. Schuerch, H. U. Structural Analysis of Swept, Low Aspect Ratio, Multi-Spar Aircraft Wings. Aeronautical Engineering Review, p. 34, November 1952.Google Scholar
4. Stein, M. and Sanders, J. L. A Method for Deflection Analysis of Thin Low-Aspect- Ratio Wings. N.A.C.A. T.N. 3640, June 1956.Google Scholar
5. Williams, D. A General Method (Depending on the Aid of a Digital Computer) for Deriving the Structural Influence Coefficients of Aeroplane Wings. Parts I and II. R. ɢ M. 3048, May 1956.Google Scholar
6. Benscoter, S. U. and Macneal, R. H. Equivalent Plate Theory for a Straight Multi-Cell Wing. N.A.C.A. T.N. 2786, September 1952.Google Scholar