Tension fields in originally curved, thin sheets during shearing stresses:

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 wit...

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Bibliographic Details
Main Author: Wagner, H. (Author)
Format: Electronic eBook
Language:English
Published: Washington, D.C National Advisory Commitee for Aeronautics 1935
Series:United States / National Advisory Committee for Aeronautics: Technical memorandum 774
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Online Access:Volltext
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
Item Description:"August 1935. - Includes bibliographical references. - NACA TM No. 774. - Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics. - Use copy Restrictions unspecified star MiAaHDL
Physical Description:1 Online-Ressource (11 p., 2 unnumbered pages)
ISBN:9781680156577

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