机翼弯度,wing bending
1)wing bending机翼弯度
英文短句/例句
1.camber changing flap改变机翼弯度的襟翼
2.Effect of Aerofoil Camber on Airfoil Aerodynamic Performance风力机的翼型弯度对风力机翼型气动性能的影响
3.For straight-winged tailless airplanes, only the negative camber satisfies the conditions for flight.对直机翼无尾飞机，只有负弯度才满足飞行条件。
4.Influence of chordwise bending stiffness on aeroelastic characteristics of flexible high-aspect-ratio wing水平弯曲刚度对大展弦比机翼颤振的影响
5.Development of a morphing wing with adaptive capability采用智能材料的变弯扭机翼实验研究
6.Subsonic Multi-point Design of A Reflex Foil Based on Genetic Algorithm基于遗传算法的负弯度翼型亚音速多点设计
7.The flexibility is all in the wing and it bends without twisting.柔性只出现在机翼上，且只有弯曲而没有扭转。
8.Press brake--Testing of the accuracyGB/T14349-1993板料折弯机精度
9.(especially of aircraft wings) angled rearward from the point of attachment.（尤指飞机机翼）从连接点向后转变角度。
10.They carefully lowered Jet into the water and suddenly, with a splash, those bent wings helped her make a flight.他们小心翼翼地把“喷气机”放进水里。突然，随着一阵溅泼声，那两个弯曲的翅膀使它飞了起来。
11.Experimental Investigation on Aerodynamic Interactions of Canard Rotor/Wing Aircraft in Hover and Low Speed Forward Flight鸭式旋翼/机翼飞机悬停及小速度前飞气动干扰实验研究
12.Either of two movable flaps on the wings of an airplane that can be used to control the plane"s rolling and banking movements.飞机的副翼飞机双翼上可以移动的两个副翼中的任一个，用来控制飞机的摇晃和转弯时的倾斜运动
13.Research on the Kinematic Simulation of a Flapping Wing Mechanism with Two Degree of Freedom两自由度扑翼机构及其运动仿真研究
14.fuselage-wing-tail combination configuration机身－机翼－尾翼组合体
15."King"s Indian, Fianchetto without c4"王翼印度,侧翼象无c4
16.If the wings are swept back, the plane will be faster.如果机翼向后斜一点，飞机速度将会更快。
17.main foil flap hydraulic actuator主翼襟翼液压执行机构
18.Slowly, carefully, he bent his knees and then sprang for the goal.慢慢地、小心翼翼地弯下膝盖，接着跳起来投篮。
相关短句/例句
camber changing flap改变机翼弯度的襟翼
3)aerofoil camber翼型弯度
4)variable camber adaptive wing变弯度自适应机翼
1.Making aircraft wing vary under different flying speeds is a key technology ofvariable camber adaptive wing.实现机翼在不同的飞行状态下的最优气动外形是变弯度自适应机翼的一项关键技术。
5)reflex foil负弯度翼型
1.Forreflex foil used in Blended Wing Body plane,when utilizing a single point design optimization to design an airfoil,a problem about the Absent consideration at off-design point often arises.针对飞翼布局飞机常用的负弯度翼型在单点优化设计时,缺乏对非设计点气动性能考虑的问题,建立了基于遗传算法的亚音速翼型多点设计优化平台,并将其应用于一个负弯度翼型的2点设计优化过程;结果表明,优化后的翼型与初始翼型相比,在巡航设计点和待机设计点的性能分别有了一定程度的改善,实现了多点设计的目的,也说明了所建立的翼型设计平台的可行性,为飞翼布局飞机的设计发展提供了良好的基础。
6)beam bender[航]翼梁折弯机
延伸阅读
自适应自整定调节分子式：CAS号：性质：在调节系统中，对象的动态特性往往是变化的,如果变化不大或调节的质量要求不高时，可以采用固定规律的调节器，假若变化大，质量要求又高时，需要选择可变规律调节器。调节器参数的改变是直接按照对象特性的变化进行的，叫作自适应调节。对象的识别和调节器的规律的计算都用一个计算装置进行，就叫自适应自整定调节，或简称自整定调节。
