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Face Wrinkling and Core Strength in Sandwich Construction

Published online by Cambridge University Press:  04 July 2016

Extract

The effect of initial waviness on the wrinkling of faces in sandwich construction is studied. Formulae are derived to determine the failing stress when the faces wrinkle due to failure of the core in tension, compression or shear. The importance of core strength requirements in maintaining surface smoothness is noted. A comparison of theory with experiments is made, and the agreement between the two is found to be reasonably good.

A sandwich construction consists of two thin face layers of high-strength material and a thick core layer of lightweight material. The function of the core is twofold. Firstly, it increases the bending rigidity of the faces and second, it stabilises them so that they will not wrinkle until high stress is reached.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1960

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References

1.Gough, G. S., Elam, C. F. and de Bruyne, N. A. (1940). The Stabilisation of a Thin Sheet by a Continuous Supporting Medium. Journal of the Royal Aeronautical Society, Vol. 44, No. 349>, pp. 1243, January 1940.CrossRefGoogle Scholar
2.Hoff, N. J. and Mautner, S. E. (1945). The Buckling of Sandwich Type Panels. Journal of the Institute of Aeronautical Sciences, Vol. 12, No. 3, pp. 285-297, July 1945.Google Scholar
3.Williams, D. (1947). Sandwich Construction—A Practical Approach for the Use of Designers. R.A.E. Rep. No. Structures 2, April 1947.Google Scholar
4.Yusuff, S. (1955). Theory of Wrinkling in Sandwich Construction. Journal of the Royal Aeronautical Society, Vol. 59, No. 529, pp. 3036, January 1955.Google Scholar
5.Wan, C. C. (1947). Face Buckling and Core Strength Requirements in Sandwich Construction. Journal of the Aeronautical Sciences, Vol. 14, No. 9, pp. 531539, September, 1947.Google Scholar
6. Strength of Metal Aircraft Elements. ANC-5 Bulletin, June 1951.Google Scholar
7.Troxell, W. W. and Engel, H. C. (1947). Column Characteristics of Sandwich Panels Having Honeycomb Cores. Journal of the Aeronautical Sciences, Vol. 14. No. 7, pp. 413421, July 1947.Google Scholar
8.Boller, K. H. (1947). Buckling Loads of Flat Sandwich Panels in Compression—With Edges Simply Supported. USDA-Forest Products Laboratory Report No. 1525-A. 1947.Google Scholar
9.Boller, K. H. (1947). Preliminary Report on the Strength of Flat Sandwich Plates in Edgewise Compression. USDA-Forest Product Laboratory Report No. 1561, 1947.Google Scholar