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NASA NTRS ยท 19850012855

Advanced stress analysis methods applicable to turbine engine structures

Abstract

Advanced 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.

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BibTeXRIS

Pian, T. H. H.. 1985-03-01. Advanced stress analysis methods applicable to turbine engine structures. https://ntrs.nasa.gov/citations/19850012855

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