Local Aerodynamic Shape Optimum Design for Axisymmetric Nose Based on Cubic Spline

WANG  Wei; CHEN  Zhihua

doi:10.15892/j.cnki.djzdxb.2011.03.032

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2011, Vol. 31 ›› Issue (3) : 177-179. DOI: 10.15892/j.cnki.djzdxb.2011.03.032

BALLISTIC AND AIRDYNAMICS

Local Aerodynamic Shape Optimum Design for Axisymmetric Nose Based on Cubic Spline

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2011, 31(3): 177-179 https://doi.org/10.15892/j.cnki.djzdxb.2011.03.032

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Received	Published
2010-09-30	2011-06-20
Issue Date
2025-05-30

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