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《Journal of Sichuan Ordnance》 2013-11
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A Study on Optimizing Design of Trajectory for Glide Extended-Range Projectile

CAO Hong-jin;GE Zhi-lei;No.59 Institute of China Ordnance Industry;Northwestern Polytechnical University;  
An optimizing design of sliding extended-range is researched. The gliding extended range projectile model is established. The whole ballistic include ballistic period and sliding period. Different methods are used to optimize paragraphs ballistic. The whole ballistic achieves the optimal. Taking someone glide extended-range projectile as study object,the design of trajectory is achieved maximum extendedrange. The conclusion of this study is conducive to the design of gliding extended-range projectiles in future.
【CateGory Index】: TJ012.3
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2 DING Song bin, WANG Zhong yuan, WANG Zheng lun (Power Eng. College, NUST, Nanjing, 210094 China);The Study on Horizon Gliding Range of Gliding Range-Assited Projectile With Fins[J];;2000-04
3 TU Sheng-yuan ZHANG Ben Ammunition Engineering department of Ordnance Engineering College,Shijiazhuang 050003,China WANG Jun-bo Equipment Technology Institute of Artillery and Aerial Defence,Beijing 100012,China FU Ting-wei 71521 Military Group,Xinxiang 45002,China;Simulation Research of Trajectory of Gliding Range-extended Projectile[J];Journal of Projectiles,Rockets,Missiles and Guidance;2005-SA
4 SHI Jin-guang WANG Zhong-yuan TU Si-hua ((Power Eng.College,NUST,Nanjing 210094,China);The Calculating Method on a Suitable Angle of Lift-Canards of Gliding Extended Range Projectile[J];Journal of Projectiles,Rockets,Missiles and Guidance;2005-SC
Chinese Journal Full-text Database 10 Hits
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