| 民用飞机迎角传感器及静压探测器布局验证方法 |
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| 引用本文： | 陈功,李秋捷.民用飞机迎角传感器及静压探测器布局验证方法[J].民用飞机设计与研究,2016(2):75. |
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| 作者姓名： | 陈功 李秋捷 |
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| 作者单位： | 上海飞机设计研究院,上海 201210 |
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| 摘 要： | 主要针对民用飞机迎角传感器及总静压探测器布局方案的设计及验证方法进行阐述。通过CFD仿真计算确定了适合的安装区域,并通过风洞试验对设计方案进行了验证。从迎角传感器的纵向特性及侧滑角的敏感性、静压测量的纵/ 横向变化规律分别对其进行了比较分析,获得了可靠的结果。
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| 关 键 词： | 风洞试验 迎角传感器 静压探测器 气动布局 |
Validation of Attack Angle Sensor and Static Pressure Detector Arrangement for Civil Aircraft |
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| Chen Gong,Li Qiujie.Validation of Attack Angle Sensor and Static Pressure Detector Arrangement for Civil Aircraft[J].Civil Aircraft Design and Research,2016(2):75. |
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| Authors: | Chen Gong Li Qiujie |
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| Institution: | Shanghai Aircraft Design and Research Institute,Shanghai 201210,China |
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| Abstract: | In this paper, design/validation of attack angle senor and static pressure detector was discussed. Appropriate mounting area was chosen by CFD method while wind tunnel test was utilized for validation. Longitude characteristics and sensitivity-to-slide of attack angle senor, as well as longitude/lateral stability of static pressure,were compared and analyzed to obtain reliable result. |
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| Keywords: | wind tunnel test attack angle senor static pressure detector aerodynamic arrangement |
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