2) rectangular flapping wing
矩形扑翼
1.
Numerical simulation on unsteady aerodynamics of rectangular flapping wing at low Reynolds number for micro air vehicles(MAVs);
微型飞行器低雷诺数矩形扑翼非定常气动特性的数值模拟
3) rectangular tapered wing aircraft
梯形或矩形机翼飞机
4) Rectangular Steel Tube Hollow Flange Beam
矩形钢管空翼缘梁
6) wing root bending moment
翼根弯矩
1.
The Lagrange multipliers optimization method is presented for wing+winglet configuration with constraint for lifting coefficient and wing root bending moment.
采用Lagrange乘数优化方法,约束升力系数和机翼翼根弯矩,通过修改机翼+翼梢小翼组合体的结构外形,减小机翼的诱导阻力和形状阻力,提高机翼的展向效率和升阻比的大小。
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条