Effects of elevated loading rates on mode I fracture of composite laminates using a modified wedge-insert fracture method

Composites Science and Technology - Tập 156 - Trang 39-47 - 2018
Solver I. Thorsson1, Anthony M. Waas2, Joseph Schaefer3, Brian Justusson3, Salvatore Liguore3
1Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109-2140, USA
2Chair, The William E. Boeing Department of Aeronautics and Astronautics, University of Washington, Seattle, WA 98195-2400, USA
3The Boeing Company, Berkeley, MO 63134, USA

Tài liệu tham khảo

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