Critical Combinations of Longitudinal and Transverse Direct Stress for an Infinitely Long Flat Plate with Edges Elastically Restrained Against Rotation (NACA Wartime Report L-49). PDF Download
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Category :
Languages : en
Pages :
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Author:
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Category :
Languages : en
Pages :
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Author: S. B. Batdorf
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
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A theoretical Investigation was made of the buckling of an infinitely long flat plate with edges elastically restrained against rotation under combinations of longitudinal are presented that give the critical combinations of stress for several different degrees of elastic edge restraints Including simple support and complete fixity. It was found that an appreciable fraction of the critical longitudinal stress may be applied to the plate without any reduction in the transverse compressive stress required for buckling.
Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 730
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Airplanes
Languages : en
Pages : 48
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 300
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Author: S.B. Batdorf
Publisher:
ISBN:
Category :
Languages : en
Pages : 8
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 188
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1566
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Author: Elbridge Z. Stowell
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 16
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Book Description
A simple interaction curve is presented for evaluating the conditions of combined shear and direct stress under which an infinitely long, flat plate with equal elastic restraints against rotation along the edges will become unstable. The theoretical work that led to the interaction curve is presented in the form of appendixes.
Author: S.B. Batdorf
Publisher:
ISBN:
Category :
Languages : en
Pages : 8
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