Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature
By: by S.B. Batdort, Murry Schildcrout, and Manuel Stein
Contributors: Schildcrout, Murry, author; Stein, Manuel, author; United States. National Advisory Committee for Aeronautics; Langley Aeronautical Laboratory
Series: National Advisory Committee for Aeronautics technical note -- number 1347; Technical note (United States. National Advisory Committee for Aeronautics) -- no. 1347.
Publisher: National Advisory Committee for Aeronautics
Published: 1947
Place of publication: Washington, D.C
Language: eng
Number of pages: 27
ISBN-13: 9781680156065
Subjects: Plates (Engineering); Strains and stresses; Buckling (Mechanics); Loads (Mechanics); Shear (Mechanics); Plaques (Ingénierie); Contraintes (Mécanique); Flambage (Résistance des matériaux); Charges; Cisaillement (Mécanique); Stress; Strain; Warping; Buckling; Shear stress
Description: A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates.
Notes: "Langley Memorial Aeronautical Laboratory."

Date of issue: June 1947.

Report no. NACA TN No. 1347.

Includes bibliographical references (pages 23-24)