Tension fields in originally curved, thin sheets during shearing stresses

• Main Authors: Wagner, H., (Author), Ballerstedt, W., (Author)
• Corporate Author: United States. National Advisory Commitee for Aeronautics.
• Format: 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.; elektronické knihy; electronic books
• ISBN: 9781680156577; 1680156578
• Physical Description: 1 online resource (11 pages, 2 unnumbered pages) : illustrations
• Item Description: "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.
• Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty

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.