Buckling Tests on Thin Circular Cylindrical Shells Heated Along an Axial Strip

By Bernard Ross, J. Mayers, Stanford University. Department of Aeronautics and Astronautics, A. Jaworski

Buckling Tests on Thin Circular Cylindrical Shells Heated Along an Axial Strip
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The results of buckling tests on circular cylinders heated along axial strips are presented and discussed. Calculations of critical temperature based upon the small deflection theory for thin circular cylindrical shells are included, and a comparison is made between theoretical and experimental results. Cylinders heated along axial strips of given widths have a theoretically predicted behaviour which corresponds resonably well to the behaviour obtained by experiment. Curves are included showing the variation of critical temperature with respect to heated axial strip width. (Athor).

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