Dynamic bridging mechanisms of through-thickness reinforced composite laminates in mixed mode delamination

Author:

Cui HaoORCID,Yasaee Mehdi,Hallett Stephen R.,Partridge Ivana K.,Allegri Giuliano,Petrinic Nik

Funder

EPSRC

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference31 articles.

1. Fawcett AJ, Oakes GD. Boeing transport experience with composite damage tolerance & maintenance. In: Research NIfA, editor. In: FAA workshop for composite damage tolerance and maintenance. Chicago; 2006. p. 32.

2. Miller SG, Handschuh KM, Sinnott MJ, Kohlman LW, Roberts GD, Martin RE, et al. Materials, manufacturing, and test development of a composite fan blade leading edge subcomponent for improved impact resistance. NASA/TM—2015-218340. Cleveland, Ohio: Glenn Research Center, NASA; 2015.

3. The response of laminated composite plates under low-velocity impact loading;Aslan;Compos Struct,2003

4. Finite-element simulation for modeling composite plates subjected to soft-body, high-velocity impact for application to bird-strike problem of composite fan blades;Nishikawa;Compos Struct,2011

5. Modelling soft body impact on composite structures;Johnson;Compos Struct,2003

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