附翼的英文

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"附翼"怎么读"附翼"的汉语解释用"附翼"造句

英文翻译手机版

skid fin

"附"英文翻译 attach; add; enclose
"翼"英文翻译 the wing of a bird
"附翼大厦" 英文翻译 : annex block
"附翼天线" 英文翻译 : skid-fin antenna
"和谐式附翼大厦" 英文翻译 : harmony annex block
"特别的附翼大厦" 英文翻译 : special annex wing
"【无线电】附翼天线，翅形天线。" 英文翻译 : skid-fin antenna
"和谐式一人单位附翼大厦" 英文翻译 : harmony 1-person annex block
"附议者" 英文翻译 : seconder
"附议人" 英文翻译 : resolutioner
"附庸" 英文翻译 : dependency; vassal; appendage
"附议" 英文翻译 : second a motion; support a proposal 我附议 ! i second that
"附庸风雅" 英文翻译 : (of landlords, merchants, etc.) mingle with men of letters and pose as a lover of culture; arty-crafty; hang on to the lips of men of letters; join the art or liberty cult
"附益条件" 英文翻译 : adjunction condition
"附庸风雅的" 英文翻译 : artsy
"附益" 英文翻译 : adjunction

例句与用法

Special annex wing
特别的附翼大厦
In this thesis , the control law based on adaptive filter for smart rotor with actively controlled trailing edge flap is researched
本文主要研究基于自适应滤波的主动控制后缘附翼智能旋翼控制律设计问题。
Their availability , stability , and robustness are proved by simulation on both model rotor and real rotor with the effect of the design parameters of the flap studied
对模型与真实旋翼进行仿真计算并研究后缘附翼设计参数的影响，结果表明两种方法都具有较好的有效性、稳定性和鲁棒性。
This thesis , which is devoted to the research on the smart rotor with actively controlled trailing - edge flap for hub oscillatory load reduction , offers a potential approach for the vibration reduction of helicopter
本文对带有主动控制后缘附翼的智能旋翼用于降低桨毂交变载荷进行探索性的研究，为降低直升机飞行中机体振动水平提供一条有效的新途径。
The smart rotor with active trailing edge is a new system for reducing the vibration which can adjust the air load of the blade to actively counteract the main harmonic of the force to the fuselage by controlling the deflection of the trailing edge
主动后缘附翼控制是一种较新的旋翼减振系统,它通过控制后缘附翼的偏转,调节桨叶的气动载荷,实现对机体激振力主要谐波分量的主动抵消。
In addition , the dynamic equation of the rotor with trailing edges and the 2 - x actuator has been modeled for analyzing the aerodynamic performance of the rotor . the result of the analysis tells us that the performance of the rotor with trailing edges can get a remarkable improvement
进而研究旋翼动力学模型,将推挽式双x驱动器模型作为后缘附翼的一种驱动机构,分析旋翼的气动性能,仿真运算结果表明,后缘附翼智能桨叶在各方面的性能都有显著的提高。