Title Effect of normal pressure on the critical compressive and shear stress of curved sheet / Norman Rafel and Charles W. Sandlin, Jr

Published Washington, D.C. : National Advisory Committee for Aeronautics, [1945]

Click on the following:
Knovel

Copies

Description 1 online resource (7, [8] pages) : illustrations Series Wartime Report / National Advisory Committee for Aeronautics ; no. L57 Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L57 Summary 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 Notes 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 Bibliography Includes bibliographical references Notes Print version record Subject Box beams. Aluminum alloys. Plates (Engineering) -- Curvature Loads (Mechanics) Shear (Mechanics) Buckling (Mechanics) Strains and stresses. Charts, diagrams, etc. box beams. aluminum alloy. shear stress. warping. buckling. stress. strain. diagrams. Aluminum alloys Box beams Buckling (Mechanics) Charts, diagrams, etc. Loads (Mechanics) Shear (Mechanics) Strains and stresses Form Electronic book Author Sandlin, Charles W United States. National Advisory Committee for Aeronautics. Langley Aeronautical Laboratory. ISBN 9781680156355 1680156357

Other Titles NACA Wartime Reports. Series L

  Permalink