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   直升机 在 航空航天科学与工程 分类中 的翻译结果: 查询用时:1.478秒
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直升机     
相关语句
  helicopter
    Helicopter Neural Network Control and Implementation of Handling Quality Requirements
    直升机神经网络控制与飞行品质要求的实现
短句来源
    Research on Vibration Signal Processing Techniques and Applications to Fault Diagnosis of Helicopter Gearbox
    振动信号处理技术在直升机齿轮箱故障诊断中的应用
短句来源
    Mathematical Model of Helicopter Rotor Airfoil
    直升机旋翼型面的数学模型
短句来源
    The Analysis and Control of Rotor Induced Vibration of Helicopter
    直升机全机振动分析与控制
短句来源
    The Development and Tests of Y-2 Light Helicopter
    Y-2小型直升机的研制和试验
短句来源
更多       
  helicopters
    Research on Feature Extraction for Fault Signals of Rotating Components in Helicopters Based on Higher-order Statistics
    直升机旋转部件故障特征提取的高阶统计量方法研究
短句来源
    Advanced Technology for Current Helicopters
    现代直升机的先进技术
短句来源
    OPTIMIZATION DESIGN FOR SUPPRESSING "GROUND RESONANCE" OF HELICOPTERS
    抑制直升机“地面共振”的优化设计
短句来源
    Control Law Design of Gust Response Alleviation for Helicopters
    直升机阵风响应缓和控制律设计
短句来源
    A Study on the Kinematics of Helicopters in Loop and Roll Maneuvers
    直升机的筋斗和横滚机动的运动学研究
短句来源
更多       
  a helicopter
    Analysis of Some Aerodynamic Design Problems for a Helicopter
    直升机气动设计有关问题分析
短句来源
    INTEGRATED SIMULATION MODEL OF A HELICOPTER ROTOR/ENGINE SYSTEM
    直升机旋翼/发动机一体化仿真模型
短句来源
    PRIMARY INVESTIGATION ON FLIGHT CONTROL SIMULATION OF A HELICOPTER LANDING ON SHIP
    直升机着舰飞行控制仿真研究初探
短句来源
    PRINCIPLE AND DESIGN OF A HELICOPTER MAIN ROTOR ACTIVE CONTROLLABLE LEAD - LEG DAMPER
    直升机旋翼可控阻尼减摆器原理与设计
短句来源
    Diagnose of Noise Fatigue Sources of a Helicopter
    直升机声疲劳源的诊断技术研究
短句来源
更多       
  military helicopter
    TECHNOLOGY OF MILITARY HELICOPTER MISSION EFFECTIVENESS' SYNTHETIC EVALUATION AND ITS APPLICATION
    军用直升机任务效能综合评估技术及应用
短句来源
    Improvement and Development of Foreign Military Helicopter
    国外军用直升机的改进与发展
短句来源
    The test results converted under standard conditions are given and compared with the relative requirements of the military helicopter flying quality specification HB6105-86. Lastly, the objective and reasonable conclusions have been drawn.
    给出了换算到标准条件下的试验结果,并与军用直升机飞行品质规范HB6105-86的有关要求进行了比较,并得出了结论。
短句来源
    MILITARY HELICOPTER BATTLED DAMAGE ASSESSMENT AND REPAIR
    直升机战伤评估及战伤修理
短句来源
    Development of Future Military Helicopter
    未来军用直升机技术
短句来源
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  helicopter
A model of the helicopter spatial motion was used by way of example.
      
The system embedding technology was shown to have much wider design potentialities than the current requirements on the design of the helicopter control systems.
      
The experimental results with the adaptive control on the "Helicopter" benchmark were described.
      
This will allow one to land in a prescribed range and to produce adequate conditions for the interception of the reentry spacecraft by a helicopter in order to prevent a rough landing.
      
Construction of a nonstationary nonlinear theory of helicopter rotors
      
更多          
  helicopters
The results of seal counts performed during the summer-autumn period of the years 1999-2001 in Pil'tun Bay from onboard "Zodiak" motor boats and "Mi-8" and "Mi-8MTV" helicopters have been analyzed.
      
Crashworthiness of helicopters on water: Test and simulation of a full-scale WG30 impacting on water
      
2024 aluminium alloy is commonly used for the fuselage of aircraft or helicopters because of its high strength.
      
The study indicated that the risk of scaring ringed seals into the water can be substantially reduced if small-type helicopters do not approach them closer than about 1500?m, and small fixed-winged aircraft not closer than about 500?m.
      
Disturbance of emperor penguin Aptenodytes forsteri chicks by helicopters
      
更多          
  a helicopter
This will allow one to land in a prescribed range and to produce adequate conditions for the interception of the reentry spacecraft by a helicopter in order to prevent a rough landing.
      
Calculation of the aerodynamic characteristics of a helicopter lifting rotor subjected to air gusts
      
A numerical method of calculating the unsteady aerodynamic characteristics of a helicopter lifting rotor smoothly enveloped by an air gust arriving from an arbitrary direction is proposed.
      
The properties of compressor blades of a helicopter gas-turbine engine with an experimental ionplasma coating Zr-Cr-N, are compared to those with Ti-Zr-N basic composition.
      
The coupling between variation of parameters of nondestructive testing and heating of rolling bearings associated with their operation regime in a helicopter reduction gear is demonstrated.
      
更多          
  military helicopter
Due to this fact the crashworthiness is more and more a standard requirement of a military helicopter.
      
Figure 6 illustrates an example of the avionics architecture of a military helicopter.
      
In Kocaeli Province, a military helicopter was tasked to fly over the disaster area to provide aerial photos of the damaged area.
      
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