Impact response of orthotropic composite plates predicted from a one-parameter differential equation
Author:
Affiliation:
1. FFA, Aeronautical Research Institute of Sweden, S-161 11 Bromma, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11105
Reference49 articles.
1. Comparison of the low and high velocity impact response of cfrp
2. Prediction of Impact Force and Duration Due to Low-Velocity Impact on Circular Composite Laminates
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