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Analysis of crack length and life flight cycle in center wing lower surface skin access hole aircraft with DCRACK software

机译：DCRACK软件中中心翼下表面皮孔飞机裂缝长度和寿命飞行周期分析

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Iis Siti Aisyah; Handika Rachmansyah Putra; Sri Sukarniyati;
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1. Automated ultrasonic inspection for crack detection at F-111 lower wing skin fastener holes [J] . Cayt Harding, Geoffrey Hugo, Susan Bowles Non-Destructive Testing Australia . 2007,第3期

机译：自动超声波检查以检测F-111下翼蒙皮紧固件孔处的裂纹
2. Determination Of The Fatigue Crack-growth Rate From The Fractographic Analysis Of A Specimen Representing The Aircraft Wing Skin [J] . Marcin Ciesielski, Jerzy Kaniowski, Wlodzimierz Karlinski International Journal of Fatigue . 2008,第6期

机译：从代表飞机机翼蒙皮的样品的形貌分析确定疲劳裂纹扩展速率
3. Damage Tolerance Analysis Software (DATAS) for Crack Growth Life Prediction and Residual Strength Analysis of Aircraft Structures [J] . l.S. Putra Key Engineering Materials . 2000,第期

机译：飞机结构裂纹扩展寿命预测和残余强度分析的损伤容限分析软件（DATAS）
4. Damage Tolerance Analysis of Double Hole-Opposite Crack at the Wing-Fuselage Joint of Civil Aircraft [C] . Muran Liu International Conference on Artificial Intelligence and Advanced Manufacture . 2020

机译：民用飞机机翼机身裂缝对双孔相对裂缝的损伤公差分析
5. Fatigue Crack Growth in Complex Residual Stress Fields Due to Surface Treatment and Foreign Object Damage Under Simulated Flight Cycles [D] . Zabeen, Suraiya. 2012

机译：在模拟飞行周期下，由于表面处理和异物损坏，复杂残余应力场中的疲劳裂纹扩展
6. Simulation Analysis of the Aerodynamic Performance of a Bionic Aircraft with Foldable Beetle Wings in Gliding Flight [O] . Caidong Wang, Yu Ning, Xinjie Wang, 2020

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7. Creep-age forming of AA7475 aluminum panels for aircraft lower wing skin application [O] . Inforzato Diego José, Costa Junior Paulo Roberto, Fernandez Fernando Ferreira, 2012

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8. Investigation of EMAT Base System for the Detection of Bolt Hole Type Cracks. Part I. Detection of Cracks in the Inaccessible Lower Half of Wing Lap Joints Using EMATS [R] . Vasile, C. V., Houston, R. H., Thompson, R. B. 1980

机译：用于检测螺栓孔型裂纹的EmaT基础系统研究。第一部分：利用EmaTs检测翼展接头下半部无法接触的裂纹

Analysis of crack length and life flight cycle in center wing lower surface skin access hole aircraft with DCRACK software

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