王坤, 朱清华, 肖升兴, & 侯祥民. (2018). 基于6σ设计的复合推力高速直升机总体参数多目标优化. 南京航空航天大学学报, 50(2), 207-212. https://doi.org/10.16356/j.1005-2615.2018.02.009
Chicago Style (17th ed.) Citation王坤, 朱清华, 肖升兴, and 侯祥民. "基于6σ设计的复合推力高速直升机总体参数多目标优化." 南京航空航天大学学报 50, no. 2 (2018): 207-212. https://doi.org/10.16356/j.1005-2615.2018.02.009.
MLA (9th ed.) Citation王坤, et al. "基于6σ设计的复合推力高速直升机总体参数多目标优化." 南京航空航天大学学报, vol. 50, no. 2, 2018, pp. 207-212, https://doi.org/10.16356/j.1005-2615.2018.02.009.
Warning: These citations may not always be 100% accurate.