Numerical Aerodynamic Research of Asymmetric Vortice Control Based on Tactical Missile

DONG  Guoguo; WANG  Xuezhan; WANG  Liqiang

doi:10.15892/j.cnki.djzdxb.2012.06.026

DONG Guoguo, WANG Xuezhan, WANG Liqiang

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (6) : 13-16.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (6) : 13-16. DOI: 10.15892/j.cnki.djzdxb.2012.06.026

MISSILES AND GUIDANCE TECHNOLOGY

Numerical Aerodynamic Research of Asymmetric Vortice Control Based on Tactical Missile

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2012, 32(6): 13-16 https://doi.org/10.15892/j.cnki.djzdxb.2012.06.026

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Received	Published
2012-03-15	2012-12-20
Issue Date
2025-05-29

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