| 旋转机翼飞机旋翼飞行验证平台设计 |
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| 引用本文： | 李亮明,高正红,何澳,邓阳平,田力.旋转机翼飞机旋翼飞行验证平台设计[J].航空工程进展,2013,4(4):488-492. |
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| 作者姓名： | 李亮明 高正红 何澳 邓阳平 田力 |
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| 作者单位： | 西北工业大学 航空学院 陕西 西安710072,西北工业大学 航空学院 陕西 西安710072,西北工业大学 航空学院,西北工业大学航空学院,西北工业大学 航空学院 |
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| 摘 要： | 为了更好地研究旋转机翼飞机旋翼模式下的飞行性能,针对旋转机翼飞机的特点,开展旋转机翼飞机旋翼飞行验证平台的设计,主要包括旋转机翼的结构设计、动力系统设计.通过数值计算的方法,对不同相对厚度椭圆翼型气动特性进行分析研究.建立旋转机翼悬停气动特性的估算方法,地面试验结果和计算结果的对比表明所建立的估算方法是有效的,该方法对今后开展旋转机翼飞机研究具有一定的参考价值和意义.
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| 关 键 词： | 椭圆翼型 旋转机翼 气动特性 飞行验证平台 |
| 收稿时间： | 2013/2/27 0:00:00 |
| 修稿时间： | 4/9/2013 12:00:00 AM |
Design of the helicopterStesting platform for rotor wing aircraft |
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| LI Liang-ming,GAO Zheng-hong,he ao,deng yang ping and tian li.Design of the helicopterStesting platform for rotor wing aircraft[J].Advances in Aeronautical Science and Engineering,2013,4(4):488-492. |
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| Authors: | LI Liang-ming GAO Zheng-hong he ao deng yang ping and tian li |
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| Institution: | College of Aeronautics , Northwestern Polytechnical University,College of Aeronautics , Northwestern Polytechnical University,College of Aeronautics , Northwestern Polytechnical University,College of Aeronautics , Northwestern Polytechnical University,College of Aeronautics , Northwestern Polytechnical University |
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| Abstract: | According to the characteristics of rotor wing aircraft, the helicopterSflying platform is developed that can apply to rotor wing aircraft research. Structural design of rotor wing and power system is analyzed and the calculating and comparing of aerodynamic performance of elliptic airfoils with different thickness-chord ratio using numerical calculation method is given. And in the end of this paper, the calculation and experimental investigation of rotor wing in hover is developed, the results in this paper provides some reference value for the research of rotor wing aircraft. |
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| Keywords: | rotor wing aircraft elliptic airfoils rotor wing |
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