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

• Main Author: Rafel, Norman.
• Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
• Other Authors: Sandlin, Charles W.
• Format: eBook
• Language: English
• Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
• Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L57.
• Subjects: Box beams.; Aluminum alloys.; Plates (Engineering) > Curvature.; Loads (Mechanics); Shear (Mechanics); Buckling (Mechanics); Strains and stresses.; Charts, diagrams, etc.; elektronické knihy; electronic books
• ISBN: 9781680156355; 1680156357
• Physical Description: 1 online resource (7, [8] pages) : illustrations
• Item Description: NACA Wartime Report L-57.; Originally issued as NACA as Advance Restricted Report L5B10 (March 1945).; 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

Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure.