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

Bibliographic Details
Main Authors:	Wagner, H. (Author), Ballerstedt, W. (Author)
Corporate Authors:	Knovel (Firm), United States. National Advisory Commitee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Advisory Commitee for Aeronautics, [1935]
Series:	Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 774.
Subjects:	Shells (Engineering) Thin-walled structures. Curvature. Shear (Mechanics) Strains and stresses. Electronic books.
Online Access:	Connect to the full text of this electronic book

Description
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.
Item Description:	"August 1935." NACA TM Number 774. Translated from Luftfahrtforschung. Volume 12, Number 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics.
Physical Description:	1 online resource (11 pages, 2 unnumbered pages) : illustrations.
Format:	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.
Bibliography:	Includes bibliographical references.
ISBN:	9781680156577 1680156578