1)straight-bladed直线翼
1.Observation and analysis of icing on static blade of straight-bladed vertical axis wind turbine直线翼垂直轴风力机静态叶片结冰的观测与分析
英文短句/例句
1.Influence of Blade Attachment on Performance of the Straight-bladed Vertical Axis Wind Turbine叶片附着物对直线翼垂直轴风力机性能的影响
2.A visual experiment by smoke wire way on the static flow field of a straight-bladed vertical axis wind turbine基于烟线法的直线翼垂直轴风力机静态流场可视化试验
3.Observation and analysis of icing on static blade of straight-bladed vertical axis wind turbine直线翼垂直轴风力机静态叶片结冰的观测与分析
4.Aileron servo pull rod should be vertical to the shaft of aileron basically.副翼舵机拉杆应基本上垂直于副翼转动轴线。
5.a straight line connecting the leading and trailing edges of an airfoil.连接机翼的前缘与后缘的直线.
6.blade-circle diameter直翼推进器盘面直径
7.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
8.National Front-Left Front全国阵线-左翼阵线
9.stowed rotor vehicle旋翼收藏式组合直升机
10.tandem rotors helicopter纵列式双旋翼直升机
11.velocity along rotor diameter速度沿旋翼直径的分布
12.intermeshing rotors helicopter交叉旋翼式直升飞机
13.intermeshing-rotor helicopter交叉双旋翼式直升机
14.bat-wing jersey蝙蝠翼绒线紧身衬衫
15.hydrofoil small waterplane area ship水翼小水线面面积船
16.Integrally cast body ribs, running parallel and perpendicular to the pipe axis, impart additional strength for high pressure conditions, thermal and pipe loads.整体铸造阀体翼肋，与管路轴线平行和垂直，增加了阀体强度，适用于高压环境、温和管道负载。
17.Multi body dynamic differential equations are combined with the equations of the unsteady dynamic inflow model to establish the complete unsteadily aeroelastic coupling analytical model of the tiltrotor.结合动力人流，研究了直升机模式下倾转旋翼机非线性非定常气弹耦合动力学特性。
18.Rotor-wing interaction analysis of a compound helicopter in forward flight复合式直升机前飞状态旋翼-机翼干扰计算分析
相关短句/例句
rectangular wing平直机翼
1.By solving the unsteady Euler/Navier-Stokes(NS) equation with Finite Volume Method and incorporating the grid velocity to take account of the gust influence,the gust responses on a rigid airfoil and rectangular wings are effectively calculated.最后针对攻角突然增大的阵风,对不同马赫数下不同展弦比平直机翼的阵风响应进行了数值模拟,得出的计算结果与文献中的计算结果一致。
3)straight wing直机翼
1.Structural stiffness effect of single & bi-fuselage UAV with higher aspect ratio and straight wing;无人机大展弦比直机翼单双机身布局对结构刚度的影响
2.In order to study the optimal layout about fuselage and wing based on wing bending stiffness on bi-fuselage aircraft with high aspect ratio straight wing, the authors utilized the engineering beam to model this physical problem and gave the numerical solution through the optimization tool box of MATLAB 6.为了探讨双机身大展弦比直机翼无人机中基于翼面弯曲刚度下机身与机翼的最佳布置问题, 本文采用工程梁对这一问题进行建模, 并利用MATLAB6。
4)Vertical tail垂直尾翼
5)straight wing平直翼
6)tail fin; vertical fin直尾翅翼
延伸阅读
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。
