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Implementation of Higher Order Laminate Theory Into Strain Rate Dependent Micromechanics Analysis of Polymer Matrix CompositesA procedure has been developed to investigate the nonlinear response of composite plates under large strain and high strain rate loading. A recently developed strain dependent micromechanics model is extended to account for the shear effects during impact. Four different assumptions of shear deformation effects are investigated to improve the development strain rate dependent micromechanics model. A method to determine through the thickness strain and transverse Poisson's ratio is developed. The revised micromechanics model is implemented into higher order laminate theory. Parametric studies are conducted to investigate transverse shear effects during impact.
Document ID
20040112003
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Kim, Heung Soo
(Arizona State Univ. Tempe, AZ, United States)
Zhu, Linfa
(Arizona State Univ. Tempe, AZ, United States)
Chattopadhyay, Aditi
(Arizona State Univ. Tempe, AZ, United States)
Goldberg, Robert K.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Report/Patent Number
AIAA Paper 2004-1638
Meeting Information
Meeting: 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Palm Springs, CA
Country: United States
Start Date: April 19, 2004
End Date: April 22, 2004
Sponsors: American Society of Mechanical Engineers, American Society of Civil Engineers, American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc., American Society for Composites
Funding Number(s)
CONTRACT_GRANT: NCC3-1024
WBS: WBS 714-30-02
Distribution Limits
Public
Copyright
Public Use Permitted.
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