1.
A Simplified Algorithm of Rotor Power and Pull to Determine Helicopter Performance
确定直升机性能的旋翼功率及拉力简化算法
2.
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
3.
Leading edge and trailing edge means the function of the dimmer.
飞机螺旋桨的前边缘和机翼后边缘是最能够反应调光器的功能的。
4.
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
5.
stowed rotor vehicle
旋翼收藏式组合直升机
6.
tandem rotors helicopter
纵列式双旋翼直升机
7.
velocity along rotor diameter
速度沿旋翼直径的分布
8.
spiral welded-on wing stabilizer
焊接螺旋翼片式稳定器
9.
intermeshing rotors helicopter
交叉旋翼式直升飞机
10.
intermeshing-rotor helicopter
交叉双旋翼式直升机
11.
Computations of Unsteady Aerodynamic Characteristic of Rotor Airfoil at Low Mach Numbers
旋翼翼型低Ma数动态失速特性计算
12.
Turbulence Modeling Based Flutter Derivative Identification of Wing Structures and Power Spectral Method for Gust Response Analysis;
机翼气动弹性湍流数值模拟和阵风响应功率谱法
13.
Experimental Study on Effect of Wind Rotor Blade Aerofoil Thickness on Power-output Characteristics
风轮叶片翼型厚度对功率输出特性影响的实验研究
14.
Random bifurcation and power spectrum analysis of a 2-dof airfoil with freeplay nonlinearity in pitch
具有间隙非线性的二元机翼的随机分岔和功率谱分析
15.
an autogiro is supported in flight by unpowered rotating wings.
旋翼飞机靠无动力的旋转式机翼支持其飞行。
16.
The results showed that the utilization coefficient of power reached the highest at an appropriate range of rotator width.
结果表明,在合适的旋耕进距范围内,旋耕机功率利用系数最高。
17.
Study on Rotary Ultrasonic Honing Machining Mechanism and Processing Parameter Experiment;
旋转功率超声珩磨加工机理及工艺实验研究
18.
Application of high-voltage & high-power frequency converters in contra rotating ventilators
高压大功率变频器在对旋式通风机上的应用