Hai, G.; Bin, Y.; Yunxin, W.; Zhiqi, L.; Yaoqiong, L.; Fei, D.
Integral Aircraft Wing Panels with Penetration Cracks: The Influence of Structural Parameters on the Stress Intensity Factor. Appl. Sci. 2020, 10, 4142.
https://doi.org/10.3390/app10124142
AMA Style
Hai G, Bin Y, Yunxin W, Zhiqi L, Yaoqiong L, Fei D.
Integral Aircraft Wing Panels with Penetration Cracks: The Influence of Structural Parameters on the Stress Intensity Factor. Applied Sciences. 2020; 10(12):4142.
https://doi.org/10.3390/app10124142
Chicago/Turabian Style
Hai, Gong, Yi Bin, Wu Yunxin, Liao Zhiqi, Liu Yaoqiong, and Du Fei.
2020. "Integral Aircraft Wing Panels with Penetration Cracks: The Influence of Structural Parameters on the Stress Intensity Factor" Applied Sciences 10, no. 12: 4142.
https://doi.org/10.3390/app10124142
APA Style
Hai, G., Bin, Y., Yunxin, W., Zhiqi, L., Yaoqiong, L., & Fei, D.
(2020). Integral Aircraft Wing Panels with Penetration Cracks: The Influence of Structural Parameters on the Stress Intensity Factor. Applied Sciences, 10(12), 4142.
https://doi.org/10.3390/app10124142