某联接翼飞机外形参数变化对稳定性影响的研究  

Impacts of Aerodynamic Configuration Parameters on Stabilities of Joined-Wing Aircraft

作　　者：郭卫刚[1] 贾忠湖[1] 康小伟[1] 

机构地区：[1]海军航空工程学院飞行器工程系,山东烟台264001

出　　处：《飞机设计》2007年第2期37-40,58,共5页Aircraft Design

摘　　要：确定7个变量参数构造了联接翼飞机的外形布局,应用涡格法分析了这7个外形参数的变化对联接翼飞机俯仰稳定性、滚转稳定性和航向稳定性的影响,为飞机总体设计提供了理论依据。Seven parameters are defined to construct the aerodynamic configuration of joined-wing aircraft. The vortex lattice method is used to analyze impacts of the seven parameters on pitching, rolling and yawing stabilities. These results would provide a basis for future aircraft designs.

关 键 词：联接翼飞机 外形参数 稳定性 

分 类 号：V221[航空宇航科学与技术—飞行器设计]