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Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heatingThermocryogenic buckling and stress analyses were conducted on a horizontally oriented cryogenic tank using the finite element method. The tank is a finite-length circular cylindrical shell with its two ends capped with hemispherical shells. The tank is subjected to cylindrical strip heating in the region above the liquid-cryogen fill level and to cryogenic cooling below the fill level (i.e., under thermocryogenic loading). The effects of cryogen fill level on the buckling temperature and thermocryogenic stress field were investigated in detail. Both the buckling temperature and stress magnitudes were relatively insensitive to the cryogen fill level. The buckling temperature, however, was quite sensitive to the radius-to-thickness ratio. A mechanical stress analysis of the tank also was conducted when the tank was under: (1) cryogen liquid pressure loading; (2) internal pressure loading; and (3) tank-wall inertia loading. Deformed shapes of the cryogenic tanks under different loading conditions were shown, and high-stress domains were mapped on the tank wall for the strain-gage installations. The accuracies of solutions from different finite element models were compared.
Document ID
19950011002
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ko, William L.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
H-1955
NAS 1.15:4579
NASA-TM-4579
Report Number: H-1955
Report Number: NAS 1.15:4579
Report Number: NASA-TM-4579
Accession Number
95N17417
Funding Number(s)
PROJECT: RTOP 505-70-63
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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