Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress
By: Elbridge Z. Stowell and Edward B. Schwartz
Contributors: Schwartz, Edward B.; United States. National Advisory Committee for Aeronautics; Langley Aeronautical Laboratory
Series: Wartime Report / National Advisory Committee for Aeronautics -- no. L340; Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L340.
Publisher: National Advisory Committee for Aeronautics
Published: 1943
Place of publication: Washington, D.C
Language: eng
Number of pages: 16
ISBN-13: 9781680156478
Subjects: Plates (Engineering); Shear (Mechanics); Buckling (Mechanics); Loads (Mechanics); Strains and stresses; Charts, diagrams; Plaques (Ingénierie); Cisaillement (Mécanique); Flambage (Résistance des matériaux); Charges; Contraintes (Mécanique); Tableaux, graphiques; Shear stress; Diagrams
Other titles: NACA Wartime Reports. Series L.
Description: A simple interaction curve is presented for evaluating the conditions of combined shear and direct stress under which an infinitely long, flat plate with equal elastic restraints against rotation along the edges will become unstable. The theoretical work that led to the interaction curve is presented in the form of appendixes.
Notes: NACA Wartime Report L-340.

Originally issued as NACA as Advance Restricted Report L3K13 (November 1943).

Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.

Includes bibliographical references.