| 低速风洞大攻角张线式支撑系统 |
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| 引用本文： | 杨恩霞,刁彦飞,庞永刚. 低速风洞大攻角张线式支撑系统[J]. 应用科技, 2001, 28(1): 4-5 |
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| 作者姓名： | 杨恩霞 刁彦飞 庞永刚 |
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| 作者单位： | 哈尔滨工程大学 机电学院，黑龙江 哈尔滨 150001 |
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| 摘 要： | 基于传统的风洞试验支撑系统，设计了能减小支架干扰的大攻角张线式支撑系统。该系统能解决支架的支撑刚度与气动干扰之间的矛盾。
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| 关 键 词： | 大攻角 飞行器 支架干扰 风洞试验 风洞 张线式支撑系统 |
| 文章编号： | 1009-671X(2001)01-0004-02 |
| 修稿时间： | 2000-11-06 |
Bracing System of LargeAttack Angle in Low Speed Wind Tunnel |
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| YANG En-xia,DIAO Yan-fei,PANG Yong-gang. Bracing System of LargeAttack Angle in Low Speed Wind Tunnel[J]. Applied Science and Technology, 2001, 28(1): 4-5 |
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| Authors: | YANG En-xia DIAO Yan-fei PANG Yong-gang |
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| Abstract: | Based on traditional bracing system of wind tunnel testing, a system of hanging brace of large angle of attack was designed, which can reduce frame interference. The contradiction between bracing rigidity and aerodynamic interference can be resolved by this system. |
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| Keywords: | hanging brace large angle of attack frame interference |
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