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A mechanics framework for a progressive failure methodology for laminated compositesA laminate strength and life prediction methodology has been postulated for laminated composites which accounts for the progressive development of microstructural damage to structural failure. A damage dependent constitutive model predicts the stress redistribution in an average sense that accompanies damage development in laminates. Each mode of microstructural damage is represented by a second-order tensor valued internal state variable which is a strain like quantity. The mechanics framework together with the global-local strategy for predicting laminate strength and life is presented in the paper. The kinematic effects of damage are represented by effective engineering moduli in the global analysis and the results of the global analysis provide the boundary conditions for the local ply level stress analysis. Damage evolution laws are based on experimental results.
Document ID
19930068777
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harris, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Allen, David H.
(NASA Langley Research Center Hampton, VA, United States)
Lo, David C.
(Texas A & M Univ. College Station, United States)
Date Acquired
August 16, 2013
Publication Date
October 1, 1989
Subject Category
Structural Mechanics
Meeting Information
Meeting: American Society for Composites, Technical Conference
Location: Blacksburg, VA
Country: United States
Start Date: October 3, 1989
End Date: October 6, 1989
Sponsors: American Society for Composites
Accession Number
93A52774
Distribution Limits
Public
Copyright
Other

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