机译:面外载荷下针迹密度和线迹厚度对缝合复合材料破坏进程和破坏特性的影响
School of Aeronautics and Astronautics, Purdue University, Armstrong Hall, West Lafayette, IN 47907, USA;
Advanced Composite Research Centre, Japan Aerospace Exploration Agency, 6-13-1 Osawa, Mitaka, Tokyo 181-0015, Japan;
Department of Aerospace Engineering, Tokyo Metropolitan University, 6-6 Asahigaoka, Hino, Tokyo 191-0065, Japan;
Advanced Composite Research Centre, Japan Aerospace Exploration Agency, 6-13-1 Osawa, Mitaka, Tokyo 181-0015, Japan;
Department of Aerospace Engineering, Nagoya University, Furoh, Chikusa, Nagoya 464-8603, Japan;
B. Delamination; B. Fracture; C. Fiber bridging; D. Non-destructive testing; Stitched composites;
机译:线迹密度和线迹厚度对Vectran缝合复合材料II型分层性能的影响
机译:线迹密度和线迹厚度对冲击强度和复合材料响应后压缩的影响
机译:3D缝合的碳/环氧树脂复合材料的制备,性能和失效,无缝合纤维损坏
机译:针脚密度和针脚厚度对Vectran缝合复合材料低速冲击响应的影响
机译:厚缝对复合材料层压板的屈曲和冲击响应的影响。
机译:床垫针迹—婴幼儿大周膜室间隔缺损的手术闭合中的改良浅缝针迹
机译:通过使用带有单针螺纹的张力试验标本缝合CFRP层压板的通过厚度负载下的机械性能研究
机译:缝合无纺石墨/环氧复合材料压缩 - 压缩疲劳载荷下的损伤发展