1)wing[英][w??][美][w??]机翼
1.Modeling and analytical investigation on rotor/wing aerodynamic interaction for tiltrotor aircraft;倾转旋翼机旋翼对机翼气动干扰的建模及分析
2.A method of coupled aerodynamic/structural integration optimization for transport-wing design;一种考虑气动弹性的运输机机翼多学科优化方法
3.Calculated method and parametric effect investigation of wing download of tiltrotor aircraft;倾转旋翼机机翼向下载荷的计算方法及参数影响分析
英文短句/例句
1.fuselage-wing-tail combination configuration机身－机翼－尾翼组合体
2.camber changing flap改变机翼弯度的襟翼
3.Influence of wing location on rotor-wing interaction of compound helicopter机翼位置对复合式直升机旋翼-机翼干扰的影响
4.An airplane with only one pair of wings.单翼机只有一对机翼的飞机
5.An airplane with wings placed above each other in three levels.三翼机具有三个重叠的机翼的飞机
6.aileron: hinged part of the wing of an aircraft,used to control its balance while it is flying副翼（飞机的机翼上控制飞行平衡的活动辅助翼）.
7.Calculation of the Aerodynamic Interaction between Rotor／Wing／Fuselage of Tilt-Rotor;倾转旋翼飞行器旋翼/机翼/机身气动干扰计算
8.the sleek swept wings of the plane.飞机有后掠翼的圆滑的机翼。
9.The ailerons on an airplane are hinged to the wing.飞机的副翼是用铰链装在机翼上的。
10.wing attachment机翼连接接头机翼的固定
11.Shape Parameter Optimization for Wing and Wingtip Based on RBF基于径向基函数的机翼和翼梢小翼外形优化
12.the ratio of the weight of an airplane to its wing area.机翼同飞机重量的比率。
13.Ice re-formed on the plane's wings.飞机的机翼上又结冰了.
14.the rake of a jet plane's wings.喷气式飞机机翼的倾斜
15.wing-to-fuselage fairing机翼机身接合整流带
16.total wing area机翼总面积(含机身部分)
17.airfoil control (system) combination机翼和操纵机构组合
18.In the method, such an airfoil is termed a four-segment airfoil.在方法,这种称为翼型四个部分机翼.
相关短句/例句
wings机翼
1.The residual correction design method for transonic wings with prescribed pressure distribution developed by Takanashi was modified.以Takanashi提出的“正反迭代、余量修正”的原理为基础 ,针对其当机翼上表面存在较强的超音速流动时 ,解的收敛性不好的问题 ,对Takanashi方法进行改进 。
2.In this paper, based on the second generation low order panel method, a computational method of potential flow around wings under high-lift configuration is given.本文采用第二代低阶面元法给出了一种高升力外形下机翼的位流计算方法。
3.The effects of locations and various cambers of small delta vortex generators on the maximum lift and stall angle of attack of wings are studied in the wind tunnel.对一个展长为５００ｍｍ，弦长为２５０ｍｍ，翼型为ＮＡＣＡ００１２的机翼模型，安装各种小三角翼旋涡发生器作低速风洞测力实验，研究小三角翼各种弯度和它与机翼的相对位置对机翼最大升力和失速迎角的影响。
3)airfoil[英]['e?f??l][美]['?r'f??l]机翼
1.Research on the Hydrodynamic Characters of Unsteady Airfoils and Straight-bladed Turbines;机翼非定常特性与直叶水轮机水动力性能分析
2.Numerical Analysis on a Two-degree-of-freedom Self-excited Airfoil with Asymmetry Freeplay Model;具有不对称间隙的二元机翼自激振动的数值分析
4)aerofoil[英]['e?r?f??l][美]['?r?'f??l]翼型;机翼
5)airfoil[英]['e?f??l][美]['?r'f??l]机翼，翼型
6)wing[英][w??][美][w??]翼，机翼
延伸阅读
机翼 飞机的组成部分，其主要作用是产生支持飞机重量或作机动飞行所需的举力。机翼的空气动力性能取决于机翼的外形、飞机飞行速度和飞行姿态。机翼外形用一些几何参数描述。翼的横剖面形状，称为翼型。从翼根到翼梢，翼型不一定相同。各剖面的翼弦也不一定在同一平面上，这称为机翼的扭转。机翼在顶视图上的形状称为机翼的平面形，典型的平面形如图上部所示。从一翼梢到另一翼梢的长度称为翼展，通常记为l；Cr、Ct为翼根和翼梢的弦长；机翼面积记为S； 翼展与平均弦长(S/l)之比称为展弦比(λ＝l2/S)。机翼的前缘和后缘都可以有后掠角。低速飞机和亚声速飞机的后掠角，通常是指各剖面的1/4弦长点的连线 （图中的虚线）与机翼对称面垂线之间的夹角,记为χ1/4。负的后掠角称为前掠角。超声速飞机的后掠角通常指机翼前缘的后掠角。左右两半机翼不一定在同一平面上，半翼的中间平面和横轴之间的夹角θ称为上反角(见图下部)。按展弦比,机翼可分为大展弦比机翼和小展弦比机翼；按掠角，可分为前掠机翼和后掠机翼。
