| 测定飞行推力和极曲线新方法 |
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| 引用本文： | 孙淑荣,王传煌.测定飞行推力和极曲线新方法[J].飞行力学,1992,10(2):60-68,84. |
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| 作者姓名： | 孙淑荣 王传煌 |
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| 作者单位： | 飞行试验研究院，飞行试验研究院 |
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| 摘 要： | 根据飞机在纵向运动时沿风轴方向的运动方程,重新定义飞机的推力和阻力,提出了一种新的测定飞行推力和阻力的方法,并将此法用于某型飞机的风洞与飞行试验极曲线相关性研究,取得了好的结果.
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| 关 键 词： | 推力 阻力 升力系数 阻力系数 |
A NEW METEHOD FOR DETRMING AIRPLANE FLIGHT THRUST AND DRAG POLAR |
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| Sun Shurong,Wang Chanhuang.A NEW METEHOD FOR DETRMING AIRPLANE FLIGHT THRUST AND DRAG POLAR[J].Flight Dynamics,1992,10(2):60-68,84. |
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| Authors: | Sun Shurong Wang Chanhuang |
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| Institution: | Chinese Flgiht Test Establishment |
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| Abstract: | This paper presented a new definiton of thrust/drag based on airplane longitudinal equation of motion in direction of wind axis, and developed a new method for determing airplane thrust/drag. The authors used the new method for the airplane wind tunnel/flight test drag polar correlation program, and obtained satisfactory results. |
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| Keywords: | Thrust Drag Lift oefficient Drag coefficient Correlation |
| 本文献已被 CNKI 维普 等数据库收录！ |
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