Tension fields in originally curved, thin sheets during shearing stresses
By: H. Wagner and W. Ballerstedt
Contributors: Ballerstedt, W., author; United States. National Advisory Commitee for Aeronautics
Series: Technical memorandums -- number 774; Technical memorandum (United States. National Advisory Committee for Aeronautics) -- no. 774.
Publisher: National Advisory Commitee for Aeronautics
Published: 1935
Place of publication: Washington, D.C
Language: eng
Number of pages: 11
ISBN-13: 9781680156577
Subjects: Shells (Engineering); Thin-walled structures; Curvature; Shear (Mechanics); Strains and stresses; Coques (Ingénierie); Structures à parois minces; Courbure; Cisaillement (Mécanique); Contraintes (Mécanique); Shell structures; Shear stress; Strain; Stress
Description: 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.
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.

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