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 。
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.
出处
《飞行力学》
CSCD
2003年第2期63-66,共4页
Flight Dynamics
