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带地效翼型俯仰控制技术研究
引用本文:沈冬,陈迎春,张彬乾.带地效翼型俯仰控制技术研究[J].飞行力学,2011,29(4):37-40,44.
作者姓名:沈冬  陈迎春  张彬乾
作者单位:1. 西北工业大学航空学院,陕西西安,710072
2. 西北工业大学航空学院,陕西西安710072;中国商用飞机有限责任公司上海飞机设计研究院,上海200232
摘    要:为解决飞翼布局起降状态俯仰控制能力不足问题,研究一种新型的腹部扰流板俯仰控制装置.针对带地效翼型,采用数值计算方法,研究了扰流板高度、弦向位置、偏度、迎角、离地高度等参数对俯仰与升阻性能的影响及其流动机理,给出了扰流板设计原则.研究结果表明,在地效作用下,合适的扰流板弦向位置和高度与偏度配合,可提供显著的抬头力矩增量和...

关 键 词:腹部扰流板  俯仰控制装置  地效  飞翼布局

Investigation on pitch control technique for an airfoil with ground effect
SHEN Dong,CHEN Ying-chun,ZHANG Bin-qian.Investigation on pitch control technique for an airfoil with ground effect[J].Flight Dynamics,2011,29(4):37-40,44.
Authors:SHEN Dong  CHEN Ying-chun  ZHANG Bin-qian
Institution:SHEN Dong1,CHEN Ying-chun1,2,ZHANG Bin-qian1(1.College of Aeronautics,Northwestern Polytechnic University,Xi'an 710072,China,2.Shanghai Aircraft Design and Research Institute,COMAC,Shanghai 200232,China)
Abstract:Aim to the pitch control problem of flying-wing configuration,a novel simple pitch control effector called a belly-flap is investigated to increase nose-up couple efficiently without unacceptable lift loss in this paper.Two-dimensional Reynolds-averaged Navier-Stokes calculations for various belly-flap configurations applied to an airfoil are described,and results are presented.The geometry parameters(size,location,deflection angle),ground effect and angle of attack are studied to detect their effects on th...
Keywords:belly-flap  pitch control effector  ground effect  flying-wing configuration  
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