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Tension fields in originally curved, thin sheets during shearing stresses
National Advisory Commitee for Aeronautics.
1 online resource (11 pages, 2 unnumbered pages) : illustrations.
The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings.
Translated from Luftfahrtforschung. Volume 12, Number 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics.
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Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 774