| 飞机重心允许范围设计准则 |
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| 引用本文： | 税清才,王秋萍.飞机重心允许范围设计准则[J].飞行力学,2003,21(2):63-66. |
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| 作者姓名： | 税清才 王秋萍 |
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| 作者单位： | 贵州航空工业公司,飞机设计研究所,贵州,安顺,561000 |
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| 摘 要： | 基于稳定气动布局飞机的操纵性和稳定性要求，提出飞机重心允许范围的确定需要考虑的一些准则。以某型机为例，用综合提出的设计准则及相关数据对该机的重心允许范围进行了详细计算。结果表明，按照提出的设计准则确定的重心允许范围与按经验估计的结果接近．说明所提出的设计准则是可行的。
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| 关 键 词： | 飞机 重心允许范围 设计准则 重心控制 飞行品质 |
| 文章编号： | 1002-0853(2003)02-0063-04 |
| 修稿时间： | 2002年5月24日 |
Design Criteria about Determination of Variable Range of Allowable Center of Gravity for an Aircraft |
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| SHUI Qing cai,WANG Qiu ping.Design Criteria about Determination of Variable Range of Allowable Center of Gravity for an Aircraft[J].Flight Dynamics,2003,21(2):63-66. |
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| Authors: | SHUI Qing cai WANG Qiu ping |
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| Abstract: | This paper introduces the design criteria about determination of variable range of allowable center of gravity based on demands for stability and controllability of an aircraft with stable aerodynamic layout. These criteria are used in the overall design for an aircraft. The results show that the variable range of allowable center of gravity determined by these criteria are closed to one estimated by overall weight control experiences and these design criteria are available in the aircraft design. |
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| Keywords: | flying qualities center of gravity control overall design of aircraft |
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