CREEP BUCKLING OF CYLINDRICAL SHELLS SUBJECTED TO UNIFORM AXIAL COMPRESSION
Technical Report
·
OSTI ID:4205013
The axially symmetric creep buckling of a circular cylindrical shell is investigated. A sandwich shell analogy and a biaxial creep law are used in the analysis. Two simultaneous, nonlinear differential equations are found to govern the stress distribution in and the displacement of the cylinder. A numerical example using these equations is carried out, and rhe results are presented in the form of curves. (auth)
- Research Organization:
- Brooklyn. Polytechnic Inst.
- NSA Number:
- NSA-13-020349
- OSTI ID:
- 4205013
- Report Number(s):
- PIBAL-489; AFOSR-TN-59-538; AD
- Country of Publication:
- United States
- Language:
- English
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