| 弹翼气动升力的设计方法研究 |
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| 引用本文： | 关世玺,程峰,吴伏家. 弹翼气动升力的设计方法研究[J]. 机械管理开发, 2005, 2(3): 1-2 |
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| 作者姓名： | 关世玺 程峰 吴伏家 |
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| 作者单位： | 中北大学热能与动力工程系,山西,太原,030051 |
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| 摘 要： | 介绍了气动升力模拟实验方案设计及数据处理的方法，为确定弹翼展开过程的升力、冲击、角速度和角加速度等气动力系数提供参数。
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| 关 键 词： | 气动升力 压心 翼载 曲线拟合 |
| 文章编号： | 1003-773X(2005)03-0001-02 |
| 修稿时间： | 2004-12-16 |
Study on the Design of Projectile Wing Aerodynamic Rising Pressure |
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| Guan Shixi,Cheng Feng,Wu Fujia. Study on the Design of Projectile Wing Aerodynamic Rising Pressure[J]. Mechanical Management and Development, 2005, 2(3): 1-2 |
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| Authors: | Guan Shixi Cheng Feng Wu Fujia |
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| Affiliation: | Guan Shixi Cheng Feng Wu Fujia |
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| Abstract: | According to the study on aerodynamic simulation rising pressure, the author introduces the project design, experiment and the method of data processing, and then acquires aerodynamic coefficients, aerodynamic rising pressure, impact force, angle rate and angle acceleration rate. |
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| Keywords: | Aerodynamic rising pressure Pressing core Load of projectile wing Curve fitting |
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