Plastic buckling of simply supported compressed plates

Tests were made of 14S-T6 aluminum-alloy square tubes to determine the critical compressive stress of simply supported flat plates in the plastic range. Excellent agreement is shown with with Stowell's theory for plastic buckling which is based upon a deformation theory of plasticity, close agr...

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Bibliographic Details
Main Authors: Pride, Richard A., (Author), Heimerl, George J., (Author)
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1817.
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ISBN: 9781680156157
1680156152
Physical Description: 1 online resource (22 pages) : illustrations

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Summary: Tests were made of 14S-T6 aluminum-alloy square tubes to determine the critical compressive stress of simply supported flat plates in the plastic range. Excellent agreement is shown with with Stowell's theory for plastic buckling which is based upon a deformation theory of plasticity, close agreement with two other deformation-type theories of plastic buckling and withthe secant-modulus method, and marked disagreement with a buckling theory based upon a flow theory of plasticity.
Item Description: Date of issue: April 1949.
Report no. NACA-TN-1817.
Bibliography: Includes bibliographical references (page 10)
ISBN: 9781680156157
1680156152
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