THE EFFECT OF GEOMETRIC NONLINEARITIES ON THE CREEP BUCKLING TIME OF AXIALLY COMPRESSED CIRCULAR CYLINDRICAL SHELLS

A correction is given to the small-displacement theory of the axisymmetric creep buckling of axially compressed circular cylindrical shells. The correction takes into account the possibility of a non-axisymmetric elastic snap through in agreement with Koiter's theory after a sufficient amount of axisymmetric permanent deformation has developed in consequency of creep.

• Corporate Authors:

  Stanford University

  Department of Aeronautics and Astronautics
  Stanford, CA  United States  94305
• Authors:
  • Hoff, N J
• Publication Date: 1974-4

Media Info

• Features: Figures; References;
• Pagination: 5 p.
• Serial:
  • Issue Number: 29

Subject/Index Terms

• TRT Terms: Buckling; Creep; Cylinders (Geometry); Shells (Structural forms)
• Uncontrolled Terms: Cylindrical shells
• Old TRIS Terms: Elastic shells
• Subject Areas: Marine Transportation; Materials;

Filing Info

• Accession Number: 00057114
• Record Type: Publication
• Source Agency: Ship Structure Committee
• Report/Paper Numbers: SUDAAR 416 Tech Rpt.
• Contract Numbers: N00014-67A-0112-0003
• Files: TRIS
• Created Date: Jul 31 1974 12:00AM