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Post impact compressive behavior of compositesIn this paper, the post impact compressive behavior of polymeric composites is studied both analytically and experimentally. In the analytical study, a closed-form solution is obtained for postbuckling of composites with a circular delamination. Using this solution, the reduced stiffness of the impact damaged region is calculated and the residual compressive strengths of quasi-isotropic laminates are predicted as a function of damage size. In the experimental study, in-plane displacements near the damaged region are determined by employing a micro moire interferometry technique. The strain concentrations as well as the compression-after-impact strength have been measured and compared with analytical predictions. Good agreement between the predicted results and experimental data was observed.
Document ID
19930030313
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lin, Kuen Y.
(NASA Langley Research Center Hampton, VA, United States)
Li, Rufeng
(Washington Univ. Seattle, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: ICAS, Congress, 18th, Beijing, China, Sept. 20-25, 1992, Proceedings. Vol. 2 (A93-14151 03-01)
Publisher: American Institute of Aeronautics and Astronautics, Inc.
Subject Category
Structural Mechanics
Accession Number
93A14310
Distribution Limits
Public
Copyright
Other

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