A Numerical and Experimental Investigation on Rolling Characteristics of the Missile with Curved Wings

CHENG  Yuqing; JIANG  Shengju; ZHENG  Kun; WANG  Jian

doi:10.15892/j.cnki.djzdxb.2012.05.026

CHENG Yuqing, JIANG Shengju, ZHENG Kun, WANG Jian

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (5) : 36-38.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (5) : 36-38. DOI: 10.15892/j.cnki.djzdxb.2012.05.026

MISSILES AND GUIDANCE TECHNOLOGY

A Numerical and Experimental Investigation on Rolling Characteristics of the Missile with Curved Wings

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2012, 32(5): 36-38 https://doi.org/10.15892/j.cnki.djzdxb.2012.05.026

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Received	Published
2012-03-28	2012-10-20
Issue Date
2025-05-29

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