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单词 helicopter rotor
释义

helicopter rotor

美 
英 
  • un.直升机旋翼
un.
1.
直升机旋翼

例句

释义:
1.
A support beam for connecting a lift generating wing section of a helicopter rotor blade with a rotor hub, said support beam comprising.
支持梁连接电梯发电翼的第一个直升机旋翼叶片与转子枢纽的地位,表示支持梁,包括。
www.tech-domain.com
2.
Finally, a case of BPS modeling for VE was provided with a virtual design process for helicopter rotor system.
最后,结合某型号直升机旋翼虚拟设计过程,给出了建立虚拟企业经营过程仿真模型的实例。
www.ceps.com.tw
3.
The adaptive optimal decoupling control method of helicopter rotor concordant loading system was discussed.
研究了直升机旋翼协调加载系统的自适应最优解耦控制问题。
www.dictall.com
4.
Model Helicopter Rotor Aerodynamics and Acoustics As Measured in Tow Anechoic Wind Tunnels.
在两个无回声风洞中测量时模型直升机旋翼空气动力学与声学。
www.lib.cafuc.edu.cn
5.
Correlation of Helicopter Rotor Tip Vortex Measurement.
直升机旋翼梢旋涡度量的相关。
www.lib.cafuc.edu.cn
6.
In the development and production of helicopter, rotor wing system is in a vital position.
在直升机研制生产中,旋翼系统的发展处于特别重要的地位。
www.fabiao.net
7.
A series of tests to do that were conducted on a UH-60A Blackhawk helicopter rotor in a NASA wind tunnel from January to May 2010.
而一系列试验将于2010年1月至3月NASA的风洞中、在一个UH-60A黑鹰直升机的转子上进行。
www.bing.com
8.
The flow field of the helicopter rotor is characterized by unsteady phenomena.
旋翼的流场呈现很强的非定常现象。
www.dictall.com
9.
In this paper a kind of fatigue design method of helicopter rotor system in detail engine design phase is presented.
本文介绍了工程设计阶段直升机旋翼系统部件强度设计的流程和方法。
www.dictall.com
10.
Comprehensive helicopter rotor instrumentation - A retrofit approach using miniature transducers
直升机旋翼综合检测设备:一种采用微型传感器的改装方法
lib.buaa.edu.cn
1.
Analysis of Kinematics and Parameters for a Nonlinear Hydraulic Damper of Helicopter Rotor
直升机旋翼非线性液压减摆器几何耦合及参数影响分析
service.ilib.cn
2.
Aeroelastic Stability for Helicopter Rotor Blades with Consideration of Transverse Shear Deformation and Warping
考虑剪切和翘曲影响的直升机旋翼气弹稳定性分析
ilib.cn
3.
Model experiment and damping identification for aeroelastic stability of helicopter rotor with elastomeric lag damper
带粘弹减摆器旋翼系统气弹稳定性试验与阻尼识别
ilib.cn
4.
Computational vorticity capturing - Application to helicopter rotor flows
计算涡量捕获:在直升机旋翼流计算中的应用
lib.buaa.edu.cn
5.
Euler solutions of transonic flow for a helicopter rotor in hover using multigrid method
用多重网格方法计算旋翼跨声速无粘流场
www.ilib.cn
6.
Analysis of Aeroelastic Stability for Helicopter Rotor with Different Elastomeric Lag Damper Connections
不同粘弹减摆器连接形式下的旋翼系统气动弹性稳定性分析
www.ilib.cn
7.
A Theoretical Basis for Diagnosis of Helicopter Rotor Imbalance Fault Using Only Information from Fuselage Vibrations
用机体振动信号诊断旋翼不平衡故障的理论基础
www.ilib.cn
8.
Study on Test, Data Acquisition and Processing Methods in Aerodynamics and Dynamics Experiments of Helicopter Rotor Model
直升机旋翼模型气动与动力学特性试验的测试与采集处理方法研究
ilib.cn
9.
Nonlinear Equivalent Damping Identification for Helicopter Rotor
直升机旋翼非线性等效阻尼的识别
ilib.cn
10.
Permanent-mold casting and foundry technique for helicopter rotor counterbalance component of copper alloy
铜合金直升机旋翼配重构件的金属型铸造及工艺
service.ilib.cn
1.
Novel Helicopter Rotor Imbalance Fault Diagnosis Using only Information from Fuselage Vibration
用机体振动诊断旋翼失衡故障方法研究
www.ilib.cn
2.
Aeroelastic Response Analysis of Helicopter Rotor During Shipboard Operation
舰面直升机旋翼瞬态气弹响应分析
ilib.cn
3.
Prediction of Aerodynamic Interactions of Helicopter Rotor on its Fuselage
直升机旋翼对机身气动干扰的计算
ilib.cn
4.
Efficient Method for Helicopter Rotor Transient Aerodynamic Response
直升机旋翼瞬态气动响应分析的一个高效方法
service.ilib.cn
5.
Aerodynamic characteristics of helicopter rotor
旋翼空气动力特性
www.baisi.net
6.
On Helicopter Rotor-blade Modulation of HF Antenna Electromagnetic Behavior Using Method of Moments
用矩量法研究直升机高频天线电磁特性的旋翼调制效应
www.ilib.cn
7.
Study on equivalent damping calculation for hydraulic damper of helicopter rotor
直升机桨叶液压减摆器等效阻尼计算研究
service.ilib.cn
8.
Research of Calibration Method of Helicopter Rotor Track and Dynamic Balance Measuring System
直升机旋翼锥体和动平衡测量仪校准方法研究
www.ilib.cn
9.
Novel Method for Diagnosis of Helicopter Rotor Compound Imbalance Fault by Using Fuselage Vibrations
用机体振动诊断直升机旋翼复合不平衡故障研究
168.160.184.82:8080
10.
Influence of downwash turbulence from armed helicopter rotor to launching of air-to-air missile
武装直升机旋翼下洗流对空空导弹发射的影响
scholar.ilib.cn
1.
Aeroelastic Stability Analysis of Helicopter Rotor Blade with Swept Tips
直升机后掠桨尖旋翼气弹稳定性研究
ilib.cn
2.
Advances in Computational Fluid Dynamics of Helicopter Rotor
直升机旋翼计算流体力学的研究进展
www.ilib.cn
3.
Application of Planar CCD to the Measurement of Helicopter Rotor Common Taper
应用CCD成像技术测量直升机旋翼共锥度
www.ilib.cn
4.
Natural Frequency of Coupled Helicopter Rotor-Fuselage
直升机旋翼与机身耦合固有频率分析
www.ilib.cn
5.
Analysis and Simulation of Electric Power Drive System in Helicopter Rotor Test Bed
直升机旋翼试验塔电力拖动系统特性分析与仿真计算
service.ilib.cn
6.
On Improving HSI Noise Prediction for Helicopter Rotor in Forward Flight When Flowfield is Partially near Sonic Speed
旋翼前飞气动噪声高效数值算法研究
www.ilib.cn
7.
Progress of Helicopter Rotor Aerodynamics
直升机旋翼空气动力学的发展
service.ilib.cn
8.
Control of chaotic oscillation for helicopter rotor blade
直升机桨叶混沌振动控制
www.ilib.cn
9.
A method of spatial distribution of helicopter rotor induced velocity
旋翼诱导速度空间分布的一种计算方法
service.ilib.cn
10.
Parametric Analysis of Inter-Blade Lag Dampers of Helicopter Rotor
直升机旋翼叶间减摆器的参数影响分析
www.ilib.cn
1.
Study on Simulation Modeling for Helicopter Rotor System
直升机旋翼系统仿真建模研究
ilib.cn
2.
Analysis of the modulation effect of the backscattered wave from a helicopter rotor
直升机旋翼对回波的调制效应分析
www.ilib.cn
3.
Research on Eliminating Extra Torque in Loading System of Helicopter Rotor
直升机加载抑制多余力控制研究
service.ilib.cn
4.
Diagnosis of Worn Pitch-Change-Link Rod End in Helicopter Rotor System
旋翼变距拉杆关节轴承磨损故障特征及磨损程度识别
www.ilib.cn
5.
A Overview on Investigation of Helicopter Rotor Noise
直升机旋翼噪声研究概述
ilib.cn
6.
Simulation of Damaged Lag Damper on Helicopter Rotor Test Rig
旋翼试验台减摆器失效故障的一种模拟方法
ilib.cn
7.
The Theoretic Prediction of RCS for Helicopter Rotor
直升机旋翼散射截面的理论预估
service.ilib.cn
8.
System of measuring helicopter rotor common taper using laser
利用激光技术测量直升机旋翼共锥度的系统
www.ilib.cn
9.
Laser dynamic testing system of helicopter rotor blade flap and lag angles
直升机旋翼挥舞、摆振的激光动态测试系统
www.ilib.cn
10.
Research on New Helicopter Rotor Shimmy Damper
新型直升机旋翼系统减摆阻尼器动态性能研究
ilib.cn
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更新时间:2025/1/13 20:13:23