The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges
By: Paul Seide
Contributors: Langley Aeronautical Laboratory; United States. National Advisory Committee for Aeronautics
Series: National Advisory Committee for Aeronautics -- 2679; Technical note (United States. National Advisory Committee for Aeronautics) -- no. 2679.
Publisher: National Advisory Committee for Aeronautics
Published: 1952
Place of publication: Washington, D.C
Language: eng
Number of pages: 30
ISBN-13: 9781680156249
Subjects: Plates (Engineering); Sandwich construction; Loads (Mechanics); Buckling (Mechanics); Elasticity; Plaques (Ingénierie); Construction sandwich; Charges; Flambage (Résistance des matériaux); Élasticité; Warping; Buckling; Modulus of elasticity
Description: A theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive buckling-load parameters of flat symmetrical corrugated core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges.
Notes: "Langley Aeronautical Laboratory.”

Date of issue: April 1952.

Report no. NACA-TN-2679.

Includes bibliographical references (page 19)