nacelle

Second generation low order panel method and its application for a case of nacelle

第二代低阶面元法及在动力短舱上的应用

A New Approach for the Acoustic Design of Aeroengine Nacelle

一种新的有限长等截面航空发动机短舱声学模型及数值结果

Nacelle Control of Intelligent Wind Generator Based on Fuzzy Control

基于模糊控制的智能风力发电机机舱控制

A sort of Realization on the Attitude Control System of Nacelle

高空气球吊篮姿态控制系统的一种实现

Application of Direct Current Torque Motor on the Azimuth Control System of Nacelle

直流力矩电动机在气球吊篮方位控制系统中的应用

Strength and mode analysis of wind turbine nacelle chassis with finite element method

风力发电机组机舱底座强度与模态分析

Numerical Simulation of Nacelle Flow and Temperature Field

直升机动力舱流场及温度场的模拟

Numerical Simulation Study on Flow Field and Temperature Field of Accessory Nacelle on a Helicopter

直升机附件舱流场和温度场的数值仿真研究

Design and Calculation of Nacelle Cover of 3D Sandwich Composites for Wind Power

3D夹层结构复合材料风电用机舱罩设计计算

Simulation Study on Helicopter Nacelle Ventilation Cooling System

直升机动力舱通风冷却系统仿真

Simulation Study of Helicopter Nacelle Ventilation Cooling System Considering of Downwash Flow

基于旋翼下洗流场的直升机动力舱通风冷却系统仿真

A full digital control system with PC / 104 in nacelle decoupling mechanism is introduced .

介绍用PC/104实现高空气球吊篮反捻机构的全数字控制系统。

Full Digital Decoupling Control System of Nacelle

高空气球吊篮的全数字反捻控制系统

Study of Electromagnetic Compatibility of Antenna System in Airborne Nacelle Jammer

机载吊舱式干扰机天线系统EMC研究

The calculation models of flow and heat transfer of helicopter nacelle are created ;

在此基础上，建立了某型直升机短舱流动和换热的计算模型，数值计算了直升机工作在地面最大状态下短舱内部的流动和换热。

The nacelle was simplified to a rigid body with general motion .

机舱简化为刚体，具有刚体一般运动。

Purchase and use of electric nacelle of rental enterprises

租赁企业电动吊篮的购置与使用

Numerical Complex Flowfield Simulation of Wing / body / Pylon / Nacelle Configuration

机翼-机身-挂架-短舱复杂流场数值模拟

Flight control of tiltrotor aircraft in helicopter mode with nacelle tilting

倾转旋翼飞机直升机模态短舱倾转飞行控制

The principle of the airborne nacelle jammer is summarized in this paper .

针对机载吊舱式干扰机的研制特点，总结和说明了该干扰机的特点和设计的原理。

Aircraft nacelle comprises engine , engine casing and accessories .

飞机发动机短舱包容了发动机、机匣、以及各种发动机附件。

The stratospheric nacelle attitude control system is the key technology in keeping position stabilization and posture adjustment .

气球吊篮姿态控制系统是吊篮在空中保持姿态稳定、进行姿态调整的关键部件。

Aeroelastic response analysis of coupled rotor / nacelle / tower for a horizontal axis wind turbine

风力发电机耦合转子/机舱/塔架的气弹响应

The finite elements model of the nacelle is created using the non-structure grids by the finite volume method .

该文利用有限体积法，应用非结构网格，建立了×型直升机发动机舱的有限元模型；

The shape and internal structure of the nacelle are very complex , Geographical simplification is necessary at first step .

由于其外形及内部件结构复杂，论文进行了简化并保留机舱外形、热源体及体积较大的内部件。

Results of the calculation show that pylon and nacelle have significant effect on the supercritical wing aerodynamic characteristics .

计算表明，短舱、挂架对超临界机翼的气动特性有显著的影响。

A finite difference method for computing the axisymmetric , transonic flows over nacelle is presented in this paper .

本文考虑轴对称跨音速进气道外流场的有限差分计算方法。

The cooling research of nacelle

发动机短舱冷却的计算研究

Different nacelle with deeper ross-section and intake over propeller shaft .

发动机舱、螺旋桨轴处的进气口有一些不同。

A Study on High-Speed Aerodynamic Intergration of the Supercritical Wing and Rear-Mounted Nacelle Configuration

超临界机翼&尾吊短舱布局高速气动综合研究