A variant of the swept-back wing is the delta wing . 后掠翼的变型是三角翼。
Numerical simulation of internal pressure fields in skew - swept impeller 弯掠翼叶轮内流压力场的计算机数值仿真
Flow characteristics and its melioration of swept wing body interference 后掠翼身干扰区流动特性及改善措施研究
Evolution of wave - packet in three - dimensional boundary layer on aswept wing 波包在后掠翼三维边界层中的演化特征
Numerical simulation of internal secondary vortex in skew - swept impellers 弯掠翼叶轮内流二次涡系的计算机数值仿真
Variable sweep aerofoil 可变后掠翼
Backswept wing aircraft 后掠翼飞机
Variable sweep wing 可变后掠翼
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。
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。
