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  United States  94305
• Authors:
  • Benoit, M
  • Hoff, N J
• Publication Date: 1973-7

Media Info

• Features: References;
• Pagination: 9 p.

Subject/Index Terms

• TRT Terms: Axial loads; Buckling; Creep; Cylinders (Geometry); Shells (Structural forms)
• Uncontrolled Terms: Axial loading; Cylindrical shells
• Subject Areas: Marine Transportation; Materials;

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