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Computational Implementation of a Thermodynamically Based Work Potential Model For Progressive Microdamage and Transverse Cracking in Fiber-Reinforced LaminatesA continuum-level, dual internal state variable, thermodynamically based, work potential model, Schapery Theory, is used capture the effects of two matrix damage mechanisms in a fiber-reinforced laminated composite: microdamage and transverse cracking. Matrix microdamage accrues primarily in the form of shear microcracks between the fibers of the composite. Whereas, larger transverse matrix cracks typically span the thickness of a lamina and run parallel to the fibers. Schapery Theory uses the energy potential required to advance structural changes, associated with the damage mechanisms, to govern damage growth through a set of internal state variables. These state variables are used to quantify the stiffness degradation resulting from damage growth. The transverse and shear stiffness of the lamina are related to the internal state variables through a set of measurable damage functions. Additionally, the damage variables for a given strain state can be calculated from a set of evolution equations. These evolution equations and damage functions are implemented into the finite element method and used to govern the constitutive response of the material points in the model. Additionally, an axial failure criterion is included in the model. The response of a center-notched, buffer strip-stiffened panel subjected to uniaxial tension is investigated and results are compared to experiment.
Document ID
20120009950
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Pineda, Evan J.
(Michigan Univ. Ann Arbor, MI, United States)
Waas, Anthony M.
(Michigan Univ. Ann Arbor, MI, United States)
Bednarcyk, Brett A.
(NASA Glenn Research Center Cleveland, OH, United States)
Collier, Craig S.
(Collier Research Corp. Newport News, VA, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2012
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-2012-217243
E-17999
AIAA Paper 2010-2815
Report Number: NASA/TM-2012-217243
Report Number: E-17999
Report Number: AIAA Paper 2010-2815
Meeting Information
Meeting: 51th Structures, Structural Dynamics, and Materials Conference
Location: Orlando, FL
Country: United States
Start Date: April 12, 2010
End Date: April 15, 2010
Sponsors: American Society of Mechanical Engineers, American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Society for Composites
Distribution Limits
Public
Copyright
Public Use Permitted.
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