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Shear Moduli for Flat Panels and the Effect of Flange Flexibility

Published online by Cambridge University Press:  28 July 2016

J. C. Simmons
J. C. Simmons*
Affiliation:
Technical Department, Royal Aeronautical Society
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Extract

This note describes an investigation into the secant and tangent moduli for flat panels in shear. Consideration is given to a comparatively recent analysis giving the secant modulus and comparison is made with he Society's Data Sheets.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 61 , Issue 562 , October 1957 , pp. 696 - 700
Copyright
Copyright © Royal Aeronautical Society 1957

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References

1.Royal Aeronautical Society. Structures Data Sheets 02.03.01 to 02.03.17, issued May 1941 to July 1948.Google Scholar
2. Kuhn, P., Peterson, J. P., and Levin, L. R. (1951). A Summary of Diagonal Tension. Part I—Methods of Analysis. N.A.C.A. T.N.2661, 1951.Google Scholar
3. Kuhn, P., and Peterson, J. P. (1947). Strength Analysis of Stiffened Beam Webs. N.A.C.A. T.N.1364, 1947.Google Scholar
4. Kuhn, P., Peterson, J. P., and Levin, L. R. (1952). A Summary of Diagonal Tension. Part II—Experimental Evidence. N.A.C.A. T.N.2662, 1952.Google Scholar
5. Crowther, F., and Sanderson, N. (1948). Experimental Investigation into Plate Web Spars under Shear. R.A.E. Report No. Structures 8, 1948.Google Scholar