工程科学学报 Chinese Journal of Engineering 飞机机翼缘条紧固孔细节原始疲劳质量评估方法 高志刚何宇廷马斌酵张天宇 Evaluation method of initial fatigue quality of aircraft wing flange fastener holes GAO Zhi-gang.HE Yu-ting.MA Bin-lin,ZHANG Tian-yu 引用本文： 高志刚，何宇廷，马斌麟，张天宇.飞机机翼缘条紧固孔细节原始疲劳质量评估方法)工程科学学报，2021,43(3)：442-450. doi10.13374j.issn2095-9389.2020.01.13.005 GAO Zhi-gang.HE Yu-ting,MA Bin-lin,ZHANG Tian-yu.Evaluation method of initial fatigue quality of aircraft wing flange fastener holes[J].Chinese Journal of Engineering,2021,43(3):442-450.doi:10.13374/j.issn2095-9389.2020.01.13.005 在线阅读View online::htps/ldoi.org10.13374/.issn2095-9389.2020.01.13.005 您可能感兴趣的其他文章 Articles you may be interested in 基于极限学习机ELM的连铸坯质量预测 Quality prediction of the continuous casting bloom based on the extreme learning machine 工程科学学报.2018.40(7)：815htps:ldoi.org10.13374.issn2095-9389.2018.07.007 联合多种边缘检测算子的无参考质量评价算法 No-reference image quality assessment using joint multiple edge detection 工程科学学报.2018.40(8：996htps:/doi.org10.13374.issn2095-9389.2018.08.014 基于声发射监测的316LN不锈钢的疲劳损伤评价 Fatigue damage evaluation of 316LN stainless steel using acoustic emission monitoring 工程科学学报.2018,40(4)：461 https::/1doi.org/10.13374.issn2095-9389.2018.04.009 一种提高图像对比度和视觉质量的新型区域背光算法 A novel local dimming algorithm to improve image contrast and visual quality 工程科学学报.2017,3912：1888htps:oi.org10.13374.issn2095-9389.2017.12.016 GH4169合金高温疲劳裂纹扩展的微观损伤机制 Microscopic damage mechanisms during fatigue crack propagation at high temperature in GH4169 superalloy 工程科学学报.2018.40(7)：822 https:/doi.org10.13374.issn2095-9389.2018.07.008 基于Lemaitre模型的辊式冲裁工艺断面质量分析 Analysis of sheared edge quality in rotary blanking process based on Lemaitre damage model 工程科学学报.2017,398：1198 https:/doi.org/10.13374.issn2095-9389.2017.08.009飞机机翼缘条紧固孔细节原始疲劳质量评估方法 高志刚 何宇廷 马斌麟 张天宇 Evaluation method of initial fatigue quality of aircraft wing flange fastener holes GAO Zhi-gang, HE Yu-ting, MA Bin-lin, ZHANG Tian-yu 引用本文: 高志刚, 何宇廷, 马斌麟, 张天宇. 飞机机翼缘条紧固孔细节原始疲劳质量评估方法[J]. 工程科学学报, 2021, 43(3): 442-450. doi: 10.13374/j.issn2095-9389.2020.01.13.005 GAO Zhi-gang, HE Yu-ting, MA Bin-lin, ZHANG Tian-yu. Evaluation method of initial fatigue quality of aircraft wing flange fastener holes[J]. Chinese Journal of Engineering, 2021, 43(3): 442-450. doi: 10.13374/j.issn2095-9389.2020.01.13.005 在线阅读 View online: https://doi.org/10.13374/j.issn2095-9389.2020.01.13.005 您可能感兴趣的其他文章 Articles you may be interested in 基于极限学习机(ELM)的连铸坯质量预测 Quality prediction of the continuous casting bloom based on the extreme learning machine 工程科学学报. 2018, 40(7): 815 https://doi.org/10.13374/j.issn2095-9389.2018.07.007 联合多种边缘检测算子的无参考质量评价算法 No-reference image quality assessment using joint multiple edge detection 工程科学学报. 2018, 40(8): 996 https://doi.org/10.13374/j.issn2095-9389.2018.08.014 基于声发射监测的316LN不锈钢的疲劳损伤评价 Fatigue damage evaluation of 316LN stainless steel using acoustic emission monitoring 工程科学学报. 2018, 40(4): 461 https://doi.org/10.13374/j.issn2095-9389.2018.04.009 一种提高图像对比度和视觉质量的新型区域背光算法 A novel local dimming algorithm to improve image contrast and visual quality 工程科学学报. 2017, 39(12): 1888 https://doi.org/10.13374/j.issn2095-9389.2017.12.016 GH4169合金高温疲劳裂纹扩展的微观损伤机制 Microscopic damage mechanisms during fatigue crack propagation at high temperature in GH4169 superalloy 工程科学学报. 2018, 40(7): 822 https://doi.org/10.13374/j.issn2095-9389.2018.07.008 基于Lemaitre模型的辊式冲裁工艺断面质量分析 Analysis of sheared edge quality in rotary blanking process based on Lemaitre damage model 工程科学学报. 2017, 39(8): 1198 https://doi.org/10.13374/j.issn2095-9389.2017.08.009