Title The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges / Paul Seide

Published Washington, D.C. : National Advisory Committee for Aeronautics, 1952

Click on the following:
Knovel

Copies

Description 1 online resource (30 pages) : illustrations Series National Advisory Committee for Aeronautics ; 2679 Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2679. Summary 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 Bibliography Includes bibliographical references (page 19) Notes Print version record Subject Plates (Engineering) Sandwich construction. Loads (Mechanics) Buckling (Mechanics) Elasticity. warping. buckling. elasticity. modulus of elasticity. Buckling (Mechanics) Elasticity Loads (Mechanics) Plates (Engineering) Sandwich construction Form Electronic book Author Langley Aeronautical Laboratory. United States. National Advisory Committee for Aeronautics. ISBN 9781680156249 1680156241

  Permalink