Aerodynamic Characteristics of Missile with a Deflected Angle of Forehead in Subsonic Flow

LI  Ming; CHEN  Zhigang; DONG  Surong; HOU  Xiucheng

doi:10.15892/j.cnki.djzdxb.2010.05.016

LI Ming, CHEN Zhigang, DONG Surong, HOU Xiucheng

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (5) : 147-148,152.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (5) : 147-148,152. DOI: 10.15892/j.cnki.djzdxb.2010.05.016

BALLISTIC AND AIRDYNAMICS

Aerodynamic Characteristics of Missile with a Deflected Angle of Forehead in Subsonic Flow

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(5): 147-148,152 https://doi.org/10.15892/j.cnki.djzdxb.2010.05.016

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Received	Published
2009-12-18	2010-10-20
Issue Date
2025-05-28

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