CREEP BUCKLING OF RELATIVELY THICK CIRCULAR CYLINDRICAL SHELLS COMPRESSED AXIALLY

Experimental results obtained with 31 nickel circular cylindrical shell specimens are evaluated in the light of the theory. The test results have already been reported in SUDAAR No. 415. The experimental creep buckling times obtained in axial compression at a temperature of 650 deg F were found to be in reasonable agreement with the theoretical formulas.

  • Corporate Authors:

    Stanford University

    Department of Aeronautics and Astronautics
    Stanford, CA  USA  94305
  • Authors:
    • Benoit, M
    • Hoff, N J
  • Publication Date: 1973-7

Media Info

  • Features: References;
  • Pagination: 9 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00050704
  • Record Type: Publication
  • Source Agency: Ship Structure Committee
  • Report/Paper Numbers: Tech Rpt #25
  • Contract Numbers: N00014-67A-0112-0003
  • Files: TRIS
  • Created Date: Jan 24 1974 12:00AM