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  USA  94305
  • Authors:
    • Hoff, N J
  • Publication Date: 1974-4

Media Info

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

Subject/Index Terms

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