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Advanced stress analysis methods applicable to turbine engine structuresAdvanced stress analysis methods applicable to turbine engine structures are investigated. Constructions of special elements which containing traction-free circular boundaries are investigated. New versions of mixed variational principle and version of hybrid stress elements are formulated. A method is established for suppression of kinematic deformation modes. semiLoof plate and shell elements are constructed by assumed stress hybrid method. An elastic-plastic analysis is conducted by viscoplasticity theory using the mechanical subelement model.
Document ID
19850012855
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pian, T. H. H.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-175573
NAS 1.26:175573
Report Number: NASA-CR-175573
Report Number: NAS 1.26:175573
Accession Number
85N21165
Funding Number(s)
CONTRACT_GRANT: NAG3-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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