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Creep analysis capability for stiffened panel structuresA method of analysis developed for predicting permanent cyclic creep deflections in stiffened panel structures is presented. The resulting computer program (TPSC, for Thermal Protection System Creep) applies either the time hardening or strain hardening theories of creep accumulation, using iterative techniques to determine structural rotations, creep strains, and stresses as a function of time. Deflections are determined by numerical integration of structural rotations along the panel length. The analytical approach was developed for purposes of analyzing thin gage entry vehicle metallic thermal protection system panels subjected to cyclic bending loads at high temperatures. The method is applicable to any panel subjected to bending loads. Predicted panel creep deflections are compared with results from cyclic tests of subsize and full size corrugation and rib stiffened panels. Empirical equations used in the analysis were developed for each material based on correlation with tensile cyclic creep data.
Document ID
19750048630
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cramer, B. A.
(McDonnell Douglas Astronautics Co. St. Louis, Mo., United States)
Rummler, D. R.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 75-814
Meeting Information
Meeting: AIAA, ASME, and SAE, Structures, Structural Dynamics, and Materials Conference
Location: Denver, CO
Start Date: May 27, 1975
End Date: May 29, 1975
Sponsors: SAE, AIAA, ASME
Accession Number
75A32702
Funding Number(s)
CONTRACT_GRANT: NAS1-11774
Distribution Limits
Public
Copyright
Other

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