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Low-velocity impact response of laminated beams subjected to initialstresses

✍ Scribed by SANKAR, B. V.; SUN, C. T.


Book ID
120614575
Publisher
American Institute of Aeronautics and Astronautics
Year
1985
Tongue
English
Weight
842 KB
Volume
23
Category
Article
ISSN
0001-1452

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Al~traet--A numerical method for the calculation of dynamic response of laminated composite plates under low-velocity impact is proposed. The non-linear, second-order differential governing equations are derived by the Lagrange's principle and the Hertzian contact law. The governing equations are de