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Buckling of thin cylindrical shells heated along an axial strip
Authors:B Ross  J Mayers  A Jaworski
Institution:1. Department of Aeronautics and Astronautics, Stanford University, Stanford, Calif
2. Politechnika Warszawska, Warsaw, Poland
Abstract:The results of buckling tests on circular cylinders heated uniformly 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 behaivor which corresponds reasonably well to the behavior obtained by experiment. Curves are included showing the variation of critical temperature with respect to heated axial-strip width.
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