Using static response characteristics as a tool for understanding impact response\ the in~uence of in!plane and out!of!plane boundary conditions\ the e}ect of curvature\ and the validity of linear and nonlinear plate theory are investigated for the transverse central impact on thin \_ber reinforced
โฆ LIBER โฆ
EXPERIMENT AND ANALYSISON THE RESPONSE OF CURVED LAMINATED COMPOSITE PANELS SUBJECTED TO LOW VELOCITY IMPACT
โ Scribed by Laura S. Kistler; Anthony M. Waas
- Publisher
- Elsevier Science
- Year
- 1998
- Tongue
- English
- Weight
- 311 KB
- Volume
- 21
- Category
- Article
- ISSN
- 0734-743X
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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