Critical combinations of shear and direct axial stress for curved rectangular panels

• Main Author: Schildcrout, Murry.
• Corporate Author: United States. National Advisory Committee for Aeronautics.
• Other Authors: Stein, Manuel.
• Format: eBook
• Language: English
• Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
• Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1928.
• Subjects: Plates (Engineering); Curvature.; Buckling (Mechanics); Shear (Mechanics); Strains and stresses.; elektronické knihy; electronic books
• ISBN: 9781680156164; 1680156160
• Physical Description: 1 online resource (29 pages) : illustrations
• Item Description: "August 1949."; NACA TN No. 1928.
• Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty

A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios.
Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semi-empirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design.