直升机旋翼的英文

• helicopter rotor

• "旋"英文翻译    whirl
• "翼"英文翻译    the wing of a bird
• "直升机旋翼挥舞" 英文翻译 :    helicopter flapping
• "直升机旋翼桨叶" 英文翻译 :    helicopter blade
• "直升机旋翼式桨叶" 英文翻译 :    helicopter-type blade
• "直升机旋翼试验塔" 英文翻译 :    helicopter tower
• "直升机旋翼机身系统" 英文翻译 :    helicopter rotor-fuselage system
• "旋翼直升机" 英文翻译 :    autogiro; autogyro; helicopter
• "单旋翼直升机" 英文翻译 :    single-rotor helicopter
• "双旋翼直升机" 英文翻译 :    dual-rotor helicopter; twin-rotor helicopter
• "四旋翼直升机" 英文翻译 :    four-rotor helicopter
• "次临界旋翼（直升机）" 英文翻译 :    subcritical rotor
• "刚接式旋翼直升机" 英文翻译 :    helicopter; rigid-rotor; rigid-rotor helicopter
• "喷气旋翼直升机" 英文翻译 :    tip-driven helicopter
• "四叶旋翼直升机" 英文翻译 :    four-blade rotor helicopter
• "无关节旋翼直升机" 英文翻译 :    helicopter; hingeless rotor; hingeless rotor helicopter
• "折叠式旋翼直升机" 英文翻译 :    collapsible helicopter
• "直升机反扭矩旋翼" 英文翻译 :    antitorque rotor
• "纵列双旋翼直升机" 英文翻译 :    helicopter; tandem-rotor
• "交叉式双旋翼直升机" 英文翻译 :    helicopter; intermeshing-rotor; intermeshing-rotor helicopter
• "交叉双旋翼式直升机" 英文翻译 :    intermeshing-rotor helicopter
• "同步交叉式双旋翼直升机" 英文翻译 :    synchropter
• "旋翼桨叶可折式直升机" 英文翻译 :    folding-rotor helicopter
• "压缩传动喷气旋翼直升机" 英文翻译 :    pressure jet helicopter
• "纵列式双旋翼直升机" 英文翻译 :    tandem helicopter; tandem rotors helicopter; tandem-rotor machine

• Frequency tests of helicopter rotating rotor blade
  直升机旋翼旋转状态下桨叶固有频率的测试
• Identification of helicopter rotor power transfer coefficient
  直升机旋翼功率传递系数确定方法
• Copter rotors really spin , and cockpit and doors really open
  直升机旋翼可旋转，驾驶舱门可关开！
• Analysis of rotor manipulation mechanism for unmanned micro helicopters
  微型无人直升机旋翼操纵机构设计及分析
• A new method for predicting high - speed impulsive noise generated by a helicopter rotor
  预测直升机旋翼气动噪声的新方法
• 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
• Stability of the coupled rotor - body system has long been one of basic topics of helicopter dynamics
  直升机旋翼/机体耦合动稳定性是直升机动力学设计的基本问题之一。
• As one of the basic problem of helicopter dynamics , the aeromechanical stability of the coupled rotor - body system has been paid a lot of attention
  直升机旋翼/机体耦合系统的气动机械动稳定性问题是直升机动力学的基本问题之一,长期以来一直受到人们的普遍关注。
• Therefore , in this thesis , the magneto - rheological damper ( mrfd ) was studied which is of simple structure , high reliability and self adaption
  为此,本文研究了结构简单、可靠性高并具有自适应能力的磁流变减摆器(阻尼器) ,用于控制直升机旋翼/机体耦合动不稳定性运动。
• Secondly , the environment , under that the helicopter flies and airborne weapon is launched , is analyzed . probe into helicopter wing wave produce wash and flow field tentatively
  然后，分析了直升机运动和机载武器发射的环境，初步探讨了直升机旋翼挥舞产生的洗流流场。