| 弯尾弹头的网格外形设计及气动特性工程计算 |
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| 引用本文： | 任智勇,黄礼耀,唐伟. 弯尾弹头的网格外形设计及气动特性工程计算[J]. 洪都科技, 2002, 0(1): 1-7 |
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| 作者姓名： | 任智勇 黄礼耀 唐伟 |
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| 作者单位： | 洪都航空工业集团650所;中国空气动力研究与发展中心,北京 |
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| 摘 要： | 弯尾导弹是提高导弹机动性的重要技术方案之一。本文研究了弯尾导弹的外形设计和网格生成方法,设计了导弹的几何外形。并对弯尾导弹的设计特点、网格生成技术、高超声速常规气动设计作了初步探讨。
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| 关 键 词： | 网格生成 气动特点 高超声速 |
| 修稿时间： | 2001-12-27 |
Grid Contour Design and Aerodynamic Feature Engineering Computation for Bend-tail Warhead |
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| Ren Zhiyong Huang Liyao. Grid Contour Design and Aerodynamic Feature Engineering Computation for Bend-tail Warhead[J]. Hongdu Science and Technology, 2002, 0(1): 1-7 |
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| Authors: | Ren Zhiyong Huang Liyao |
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| Abstract: | The band -tail missile is one of the im portant technical proposals to im-prove the maneuverability of the mis sile.This paper researched the bend-tail missile contour design and grid generation method,and designed the geographic c ontour of the missile.And also it made a preliminary discussion over the bend -tail mis sile design feature,grid generation technique and high supersonic conventional aerodynamic design. |
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| Keywords: | Grid Generation Aerodynamic Featur e High Supersonic |
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