Buckling of cylindrical shells under combined axial preload, nonuniform heating and torque

Author:

Ari-Gur J.,Baruch M.,Singer J.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference13 articles.

1. Hoff, N.J., “Thermal Buckling of Thin-Walled Circular Cylindrical Shells,” Stanford Univ. SUDAER No. 137 (Oct. 1962).

2. Anderson, M.S., “Combinations of Temperature and Axial Compression Required for buckling of Ring-Stiffened Cylinder,” NASA TN-D-1224 (April 1962).

3. Anderson, M.S. and Card, M.F., “Buckling of Ring-Stiffened Cylinders under a Pure Bending Moment and a Non-Uniform Temperature Distribution,” NASA TN-D-1513 (Nov. 1962).

4. Hoff, N.J., Chao, C. andMadsen, W.A., “Buckling of a Thin-Walled Circular Cylindrical Shell Heated Along an Axial Strip,”J. of App. Mech.,31 (2),253 (June1964).

5. Hoff, N.J. andRoss, B., “A New Solution of the Buckling Problem of Thin Circular Cylindrical Shells Heated Along an Axial Strip,”Recent Progress in Applied Mechanics, the Folke Odqvist Volume, Broberg, B., Hult, J. andNiordson, F., eds., Almqvist and Wiksell, Stockholm (1967).

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