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Tension fields in originally curved, thin sheets during shearing stresses

Author: H Wagner; W Ballerstedt; United States. National Advisory Commitee for Aeronautics.
Publisher: Washington, D.C. : National Advisory Commitee for Aeronautics, [1935]
Series: Technical memorandum (United States. National Advisory Committee for Aeronautics), no. 774.
Edition/Format:   eBook : Document : National government publication : EnglishView all editions and formats
Summary:
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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Genre/Form: Electronic books
Additional Physical Format: Print version:
Wagner, H.
Tension fields in originally curved, thin sheets during shearing stresses
(OCoLC)696180837
Material Type: Document, Government publication, National government publication, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: H Wagner; W Ballerstedt; United States. National Advisory Commitee for Aeronautics.
ISBN: 9781680156577 1680156578
OCLC Number: 919168137
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.
Reproduction Notes: Electronic reproduction. [S.l.] : HathiTrust Digital Library, 2010. MiAaHDL
Description: 1 online resource (11 pages, 2 unnumbered pages) : illustrations.
Details: 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.
Series Title: Technical memorandum (United States. National Advisory Committee for Aeronautics), no. 774.
Responsibility: H. Wagner and W. Ballerstedt.

Abstract:

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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