Numerical Investigation on Aerodynamic Characteristics of Missile Wing with Minimum Aspect Ratio

LI Jian, JING Daiyong

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2017, Vol. 37 ›› Issue (2) : 115-117.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2017, Vol. 37 ›› Issue (2) : 115-117. DOI: 10.15892/j.cnki.djzdxb.2017.02.028
BALLISIIC AND AIRDYNAMICS

Numerical Investigation on Aerodynamic Characteristics of Missile Wing with Minimum Aspect Ratio

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2017, 37(2): 115-117 https://doi.org/10.15892/j.cnki.djzdxb.2017.02.028

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