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机译:H-VARTM制造的缺口和缺口碳/环氧树脂复合材料的拉伸压缩疲劳行为
Department of Aeronautics and Astronautics, Air Force Institute of Technology, AFIT/ENY, Bldg. 640, 2950 Hobson Way, Wright-Patterson AFB, OH 45433-7765, USA;
Department of Aeronautics and Astronautics, Air Force Institute of Technology, AFIT/ENY, Bldg. 640, 2950 Hobson Way, Wright-Patterson AFB, OH 45433-7765, USA;
Department of Computational Science and Engineering, North Carolina A&T State University, Greensboro, NC 27411, USA;
Department of Computational Science and Engineering, North Carolina A&T State University, Greensboro, NC 27411, USA;
Department of Aerospace Engineering, Texas A&M University, College Station, TX 77843, USA;
carbon/epoxy; tension-compression fatigue; notch; circular hole; H-VARM; damage mechanisms;
机译:有缺口和无缺口[0 /±30 /±60/90] _s GFR / EPOXY复合材料在静态和疲劳载荷下的行为
机译:单轴碳/环氧复合材料离轴非线性速率相关行为中的拉伸-压缩不对称建模
机译:环境条件对含有缺陷碳/环氧树脂织式层压板轴张力 - 压缩疲劳行为的影响
机译:碳纤维增强环氧树脂复合材料(== 45)4s层压板在拉伸和拉伸-压缩疲劳疲劳试验下的疲劳行为
机译:使用紧凑和双缺口缺口拉伸压缩试样在蠕变疲劳条件下的裂纹扩展行为。
机译:拉伸-拉伸拉伸-压缩和压缩-压缩疲劳载荷下增材制造的Ti6Al4V支架的疲劳寿命
机译:角层石墨/环氧树脂复合材料的有缺口和无缺口疲劳行为
机译:真空辅助树脂传递模塑制备碳纤维/环氧树脂(Im7 / EpON 862)复合材料的拉伸 - 压缩疲劳行为