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Continuum Fatigue Damage Modeling for Critical Design, Control, and Fault Prognosis

Authors :
Lorenzo, Carl F
Publication Year :
1996
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1996.

Abstract

This paper develops a simplified continuum (continuous with respect to time, stress, etc.) fatigue damage model for use in critical design, Life Extending Control and fault prognosis. The work is based on the local strain cyclic damage modeling method. New nonlinear explicit equation forms of cyclic damage in terms of stress amplitude are derived to facilitate the continuum modelling. Stress based continuum models are derived. Extension to plastic strain-strain rate models is also presented. Progress toward a non-zero mean stress based is presented. Also new nonlinear explicit equation forms in terms of stress amplitude are derived for this case. Application of the various models to design, control, and fault prognosis is considered.

Subjects

Subjects :
Structural Mechanics

Details

Language :
English
Database :
NASA Technical Reports
Notes :
RTOP 505-62-05
Publication Type :
Report
Accession number :
edsnas.19960012202
Document Type :
Report