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The Elastic Stability of a Curved Plate Under Axial Thrusts

Published online by Cambridge University Press:  28 July 2016

S. C. Redshaw
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Extract

Theoretical critical stresses have been obtained for four cases in each of which a curved panel has been subjected to a compressive stress, parallel in direction to a generator and uniformly distributed around its top and bottom circumferential edges.

Information

Type
Proceedings
Information
The Aeronautical Journal , Volume 42 , Issue 330 , June 1938, pp. 536 - 553
Copyright
Copyright © Royal Aeronautical Society 1938

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References

1. The Theory of Sound. Lord Rayleigh, Book 1877.Google Scholar
2. Sur la Stabilité des Systèmes Elastiques. S. Timoshenko, Annales des Ponts et Chaussées, 1913.Google Scholar
3. Rayleigh's Principle, p. 28, Temple and Bickley, Book 1935.Google Scholar
4. Applied Elasticity, p. 561, Prescott, J., Book 1924.Google Scholar
5. Elastic Instability of a Thin Curved Panel. S. C. Redshaw, Aero. Res. Ctee. R. & M. 1565, 1933.Google Scholar
6. Theorie und Versuche zur Festigkeit von Schaleuriimpfen. Ebner, H., Luftfahrt- Forschung, 1937.Google Scholar
7. On the General Theory of Elastic Stability, Southwell, R. V..Google Scholar
8. On the Stability of a Plane Plate under Thrusts in its own Plane with applications to the “ buckling “ of the sides of a ship. Bryan, G. H., Proc. Lond. Math. Soc., Vol. 22, 1891.Google Scholar
9. Buckling of Thin Plates in Compression, H. L. Cox, Aero. Res. Ctee. R. & M. 1554, 1933.Google Scholar
10. Theory of Elastic Stability, p. 467, p. 339, p. 342. Timoshenko, S., Book 1936.Google Scholar
11. Report on Aircraft Materials Research. Newell, J. S. and Gale, W. H., Massachusetts Inst, of Tech., 1931–32.Google Scholar
12. Preliminary Report on the Ultimate Compressive Strength of Curved Sheet Panels. Sechler, E. E., California Inst, of Tech., Publication No. 36.Google Scholar
13. Compression Tests on Curved Panels of Thin Sheet Duralumin. Cox, H. L. and Clenshaw, W. J., Aero. Red. Ctee., Unpublished.Google Scholar
14. The Strength of Tubular Struts. A. Robertson, Aero. Res. Ctee. R. & M. 1185, 1927.Google Scholar