Buckling of Skew Plates with Continuity or Rotational Edge Restraint

Author:

Huyton P.12,York C. B.12

Affiliation:

1. PhD Candidate, Dept. of Aerosp. Engrg., Univ. of Glasgow, Glasgow, G12 8QQ, UK.

2. Sr. Lect., Dept. of Aerospace Engrg., Univ. of Glasgow, James Watt Build., Glasgow, G12 8QQ, UK. E-mail: c.york@aero.gla.ac.uk; formerly, School of Civ. and Envir. Engrg., The Univ. of Edinburgh, Crew Build., The King's Build., Edinburgh, EH9 3JN, UK.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference35 articles.

1. ABAQUS/Standard Version 5.8 . (1998). Hibbit Karlsson and Sorensen Inc.

2. Anderson M. S. Stroud W. J. Durling B. J. and Hennessy K. W. ( 1981). “PASCO: Structural panel analysis and sizing code user's manual.” NASA TM 80182 National Aeronautics and Space Administration Washington D.C.

3. Anderson R. A. ( 1951). “Charts giving critical compressive stress of continuous flat sheet divided into parallelogram-shaped panels.” NACA TN 2392 National Advisory Committee for Aeronautics Washington D.C.

4. Anderson R. A. and Semonian J. W. ( 1954). “Charts relating the compressive buckling stress of longitudinally supported plates to the effective deflectional and rotational stiffness of the supports.” NACA TN 1202 National Advisory Committee for Aeronautics Washington D.C.

5. Argyris J. H. ( 1966). “Continua and discontinua (an apercu of recent developments of the matrix displacement method).” Matrix Methods in Struct. Mech. 11–190.

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