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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.
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Tension fields in originally curved, thin sheets during shearing stresses
1935, National Advisory Commitee for Aeronautics
in English
1680156578 9781680156577
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Edition Notes
"August 1935."
NACA TM No. 774.
Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics.
Includes bibliographical references.
Restrictions unspecified
Access restricted to Ryerson students, faculty and staff.
Electronic reproduction. [Place of publication not identified] : HathiTrust Digital Library, 2010.
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212
digitized 2010 HathiTrust Digital Library committed to preserve
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