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

• Main Author: Seide, Paul, (Author)
• Corporate Authors: Langley Aeronautical Laboratory., United States. National Advisory Committee for Aeronautics.
• Format: eBook
• Language: English
• Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
• Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2679.
• Subjects: Plates (Engineering); Sandwich construction.; Loads (Mechanics); Buckling (Mechanics); Elasticity.; elektronické knihy; electronic books
• ISBN: 9781680156249; 1680156241
• Physical Description: 1 online resource (30 pages) : illustrations
• Item Description: "Langley Aeronautical Laboratory."; Date of issue: April 1952.; Report no. NACA-TN-2679.
• Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty

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.