摘要
以某型双发低速飞机为例，对剪切翼梢装置对飞机滚转性能的影响进行了理论研究和分析。结果表明，在相同结构参数和飞行状态下，采用剪切翼梢，将使飞机的滚转性能有所降低。所得结果对飞机设计、特别是飞机改型设计有一定实用价值。
In the paper, as an example by some type low speed twin-engine airplane,theoretical research and analyses about the effect of the tip unit of a sheared wing on airplaneroll performance are conducted.The results show that it will worsen the airplane rollperformance by using a “sheared wing” tip with same structure parameters and flightcondition.The result obtained will be of a certain practical value for airplane design, especially modified version design.
出处
《飞行力学》
CSCD
北大核心
1995年第1期46-50,共5页
Flight Dynamics
关键词
剪切翼梢
滚转特性
飞行品质
飞行
Sheared-tip wing Roll performance Flight quality
