Canard wing increases lift coefficient with the penalty of the increase of drag coefficient 低于主机翼的鸭翼将加强前掠翼布局的缓失速特性。
2.
Force measurement in a low speed wind tunnel was conducted to investigate the effects of the height of a distant canard wing on the longitudinal aerodynamic characteristics of a forward - swept configuration 摘要基于前掠翼鸭式前翼布局的风洞测力实验,分析了距离主机翼较远的鸭翼相对于主机翼的高度对布局纵向气动性能的影响。