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Book Cover
Author Griffith, George E., author

Title Experimental investigation of the effects of plastic flow in a tension panel with a circular hole / by George E. Griffith
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1948


Description 1 online resource (17 pages) : illustrations
Series National Advisory Committee for Aeronautics technical note ; number 1705
Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1705.
Summary Seven uniformly dimensioned 24S-T tension panels with a central circular hole were subjected to various loads in order to study the effects of plastic flow at the point of maximum stress concentration. The results, presented in graphical form, show that, as the amount of plastic flow increases, the stress concentration factor is appreciably reduced and the strain concentration factor is appreciably increased. Subjecting the panels to 100 repeated loading cycles caused no change to occur in the maximum values of the stress and strain concentration factors
Notes "September 1948."
NACA TN No. 1705
Bibliography Includes bibliographical references
Notes Master and use copy. Digital master created according to Technical Guidelines for Digitizing Archival Materials for Electronic Access. U.S. National Archives and Records Administration, 2004.$5TxDN
digitized 2011 University of North Texas committed to preserve pda TXdn
Print version record
Subject Aluminum alloys.
Plates (Engineering)
Loads (Mechanics)
Alloys -- Creep
Strains and stresses.
aluminum alloy.
Aluminum alloys.
Loads (Mechanics)
Plates (Engineering)
Strains and stresses.
Genre/Form Electronic books
Form Electronic book
Author United States. National Advisory Committee for Aeronautics.
ISBN 9781680156140