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Joints in Flat Panels Subjected to Shear and Combined Shear and Tension

F.W. David, A.F.R.Ae.S. (Mr. F. W.T David is chief designer of Commonwealth Aircraft Corp. Pty. Ltd., Melbourne, Australia)
J. Solvey, A.F.R.Ae.S. (Mr. J. Solvey design engineer of Commonwealth Aircraft Corp. Pty. Ltd., Melbourne, Australia)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 April 1947

Abstract

THIS paper deals with semi shear‐resistant panels (incomplete tension fields) subjected to pure shear—as well as combined shear and tension loads. It establishes the stresses in the midplane of the sheet and the loads acting on panel joints.

Citation

David, F.W. and Solvey, J. (1947), "Joints in Flat Panels Subjected to Shear and Combined Shear and Tension", Aircraft Engineering and Aerospace Technology, Vol. 19 No. 4, pp. 118-124. https://doi.org/10.1108/eb031494

Publisher

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MCB UP Ltd

Copyright © 1947, MCB UP Limited