The Study on Trajectory of Missile Separating from Cavity with Aerodynamic Interference Considered

TANG  Shangqin; HUANG  Changqiang; WENG  Xingwei

doi:10.15892/j.cnki.djzdxb.2013.03.046

TANG Shangqin, HUANG Changqiang, WENG Xingwei

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (3) : 138-142.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (3) : 138-142. DOI: 10.15892/j.cnki.djzdxb.2013.03.046

BALLISIIC AND AIRDYNAMICS

The Study on Trajectory of Missile Separating from Cavity with Aerodynamic Interference Considered

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2013, 33(3): 138-142 https://doi.org/10.15892/j.cnki.djzdxb.2013.03.046

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Received	Published
2012-08-24	2013-06-20
Issue Date
2025-05-26

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