Numerical Simulation for Influence of Asymmetric Wing on Rolling Moment of Small UAV

CHEN  Junkui; WANG  Zhijun; WU  Guodong; XU  Yongjie; LI  Sheshe

doi:10.15892/j.cnki.djzdxb.2016.01.003

CHEN Junkui, WANG Zhijun, WU Guodong, XU Yongjie, LI Sheshe

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2016, Vol. 36 ›› Issue (1) : 10-14.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2016, Vol. 36 ›› Issue (1) : 10-14. DOI: 10.15892/j.cnki.djzdxb.2016.01.003

MISSILES AND GUIDANCE TECHNOLOGY

Numerical Simulation for Influence of Asymmetric Wing on Rolling Moment of Small UAV

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2016, 36(1): 10-14 https://doi.org/10.15892/j.cnki.djzdxb.2016.01.003

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