Zhou, J., & Wang, S. (2018). Initial Fatigue Quality Assessment for Aircraft Wing Panel Fastener Hole. Xibei Gongye Daxue Xuebao, 36(1), 91-95. https://doi.org/10.1051/jnwpu/20183610091
Chicago Style (17th ed.) CitationZhou, Junjie, and Shengnan Wang. "Initial Fatigue Quality Assessment for Aircraft Wing Panel Fastener Hole." Xibei Gongye Daxue Xuebao 36, no. 1 (2018): 91-95. https://doi.org/10.1051/jnwpu/20183610091.
MLA (9th ed.) CitationZhou, Junjie, and Shengnan Wang. "Initial Fatigue Quality Assessment for Aircraft Wing Panel Fastener Hole." Xibei Gongye Daxue Xuebao, vol. 36, no. 1, 2018, pp. 91-95, https://doi.org/10.1051/jnwpu/20183610091.
Warning: These citations may not always be 100% accurate.