1) 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。
2) root bending moment
根部弯矩
1.
The pressure on the vertical tail surface is integrated to yield the root bending moment at each time step,then the Root Mean Square(RMS) value of the fluctuant root bending moment coefficient.
通过非定常Euler方程计算各迎角下的非定常流场及垂尾根部弯矩系数。
2.
Unsteady pressures at 9 positions on both sides of the vertical tail were recorded,and these unsteady pressures were integrated along the surface to yield the root bending moment of the vertical tail.
实验测量了垂尾内外侧表面各9处的脉动压力,并将脉动压力沿表面积分近似得到垂尾的根部弯矩响应。
3.
The test method include root bending moment measurement and tip acceleration measurement.
通过实验检验了实验方案的正确性、可行性,并通过垂尾的根部弯矩测量和翼尖加速度测量得到了双垂尾的抖振响应曲线和抖振起始迎角,掌握了边条翼布局的双垂尾抖振响应随迎角变化的规律,即在抖振起始迎角之前,双垂尾的抖振响应很小且基本不随迎角变化,当迎角超过抖振起始迎角时,抖振响应急剧增加并在某一迎角范围达到最大值,之后抖振响应逐渐降低。
4) bending moment
弯矩
1.
The problem of designating the sign of bending moment in the curvature-bending moment equation;
关于规定曲率弯矩方程弯矩正负号的问题
2.
A study of axial force and bending moment in tube numerical control bending based on finite element method;
基于有限元模拟的数控弯管过程轴力和弯矩的分析计算
3.
Study of predicting theory of cutting bending moment in orthogonal cutting;
正交切削的切削弯矩预报理论的研究
5) flexural torque
弯矩
1.
Some important mechanical phenomena are analyzed,such as the strain in the transverse direction,longitudinal direction and direction of fiber,flexural torque and longitudinal curvature during the bending process.
研究了折叠复合材料结构的成型工艺,成功地制备了碳纤维/环氧树脂、玻璃纤维/环氧树脂复合材料薄壁圆柱壳试样,并对它们的折叠弯曲性能进行了实验研究,分析了弯曲过程中横向、纵向和纤维方向三个方向的应变变化情况,以及试样在弯曲过程中的弯矩和纵向曲率变化规律。
6) Moment
[英]['məʊmənt] [美]['momənt]
弯矩
1.
Determination of a rigid frame cases without moment in concentrated loading at the joint;
刚架在结点集中力作用下无弯矩情况的判定
2.
Research on moment-curvature hysteretic behaviors of concrete filled circular steel tubes;
圆钢管混凝土构件弯矩-曲率滞回特性研究
3.
The exact formula for calculating the moment of single foundation under uniaxial eccentric load;
单向偏心荷载作用下柱下独立基础弯矩的精确计算公式
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