Effect of normal pressure on the critical compressive stress of curved sheet

• Main Author: Rafel, Norman
• Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
• Format: Electronic eBook
• Language: English
• Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
• Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L258.
• Subjects: Atmospheric pressure.; Buckling (Mechanics); Strains and stresses.; Loads (Mechanics); Charts, diagrams, etc.; elektronické knihy; electronic books
• ISBN: 9781680156348; 1680156349
• Physical Description: 1 online resource (2, [8] pages) : illustrations
• Abstract: Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress.
• Item Description: NACA Wartime Report L-258.; Originally issued as NACA as a Restricted Bulletin (November 1942).; Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
• Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty