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Continuum Fatigue Damage Modeling for Critical Design, Control, and Fault PrognosisThis 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.
Document ID
19960012202
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lorenzo, Carl F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:107065
E-9926
NIPS-96-08117
NASA-TM-107065
Report Number: NAS 1.15:107065
Report Number: E-9926
Report Number: NIPS-96-08117
Report Number: NASA-TM-107065
Meeting Information
Meeting: International Symposium on Transport Phenomena and Dynamics of Rotating Machinery
Location: Honolulu, HI
Country: United States
Start Date: February 25, 1996
End Date: February 29, 1996
Sponsors: Pacific Center of Thermal Fluids Engineering and US Turbo and Power Machinery Research Center
Accession Number
96N18439
Funding Number(s)
PROJECT: RTOP 505-62-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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