| 滑翔增程弹方案弹道特性的研究 |
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| 引用本文： | 史金光,王中原,易文俊. 滑翔增程弹方案弹道特性的研究[J]. 弹道学报, 2003, 15(1): 51-54 |
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| 作者姓名： | 史金光 王中原 易文俊 |
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| 作者单位： | 南京理工大学动力工程学院,南京,210094 |
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| 摘 要： | 阐述了滑翔增程弹的飞行原理，建立了滑翔增程弹的方案弹道模型，通过数值计算得到了滑翔增程弹方案弹道的形状特征、弹丸飞行速度沿全弹道的变化规律和最大射程角的特点，对今后进行滑翔增程弹的设计有重要促进作用。
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| 关 键 词： | 滑翔增程弹 弹道特性 弹丸 飞行速度 射程角 炮弹 |
| 修稿时间： | 2002-09-01 |
A STUDY ON THE PROJECT TRAJECTORY CHARACTE RISTICS OF GLIDING EXTENDED RANGE PROJECTILE |
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| Shi Jinguang Wang Zhongyuan Yi Wenjun. A STUDY ON THE PROJECT TRAJECTORY CHARACTE RISTICS OF GLIDING EXTENDED RANGE PROJECTILE[J]. Journal of Ballistics, 2003, 15(1): 51-54 |
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| Authors: | Shi Jinguang Wang Zhongyuan Yi Wenjun |
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| Abstract: | The flight theory of gliding extended range projectile is explained,and the project ballistic model is established.For gliding extended range projectiles,the project ballistic shape characteristics,the variation law of projectile's flight velocity along trajectory,and the characteristics of maximum range angle are gained by numerical calculation.These are conducive to the design of gliding extended range projectiles in future. |
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| Keywords: | gliding extended range projectiles project trajectory ratio between rise and resistance |
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