fuselage

The problem turned out to be metal fatigue in the fuselage .

问题原来是飞机机身出现金属疲劳。

The length of the fuselage was increased due to a degree of directional instability .

由于存在某种程度的航向不稳定性，机身被加长了。

Structure Optimization Design Study of Fuselage Main Frame

机身主要承力框结构优化设计研究

Research of Civil Composite Materials Engineering Application Validation for Helicopter Fuselage Structure

直升机机身结构用国产复合材料工程化应用验证技术研究

A time domain method for propeller noise prediction including aircraft fuselage effect

考虑飞机舱壁影响的螺旋桨声场时域预测法

Research on Load Distribution of Aircraft Wing / Fuselage Main Joints

某型飞机翼身主接头的载荷分配研究

Study of intelligent design on the fuselage model surface of the cockpit section

飞机座舱段机身曲面造型智能化设计的研究

A New Rotor / Fuselage Vibration Isolator and Its Characteristic Analysis

一种新型旋翼/机身隔振装置及其性能分析

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

Experimental Study of Aircraft Fuselage Aerodynamic Forces at High Angles of Attack

飞机机身大迎角气动力实验研究

A Design Approach to Fuselage Frames in Aircraft Upgrade Design

改型设计中飞机普通框一种设计方法

A CAD / CAE Integrated Design to Fuselage Main Frame

某承力密封框的CAD/CAE集成设计

Fatigue analysis for civil aircraft fuselage typical truss joint in serving environment

综合环境下民机机身典型长桁接头疲劳分析

Rotor / Fuselage Compound Model Wind Tunnel Test with Sideslip Angle

直升机旋翼/机身组合模型的带侧滑角风洞试验

Coupling Technique of Rotor - Fuselage Dynamic Analysis

旋翼-机身动力分析的耦合技术

Fuselage can too the customer need to be adopted four pillar type construction .

机身也可用户需要采用四柱式结构。

An Improved Method of Aerodynamic Calculation for the Fuselage of a Helicopter

直升机机身气动特性计算方法研究

Mechanical model OE landing impact of three dimensional fuselage landing gear

三维机身起落架着陆冲击力学模型

Automatic calculation of crack intensity factor of aircraft fuselage test model by sub-structure method

用子结构方法自动计算飞机舱体实验模型裂缝的应力强度因子

Introduction and Application of Φ 4m Rotor / Fuselage Compound Model Test Stand

Φ4米旋翼/机身组合模型试验台及应用

The fuselage impedance is obtained from a shake test or finite element analysis .

机身阻抗可由机身的有限元分析计算或振动试验获得。

Thermal Stress Failure on Heat Insulation Coatings for Airborne Missile Fuselage Connection

机载导弹弹体隔热层的热应力故障与对策

Analysis of Helicopter Ground Resonance with Fuselage State Feedback

带机体状态反馈的直升机地面共振分析

Study on Flow Controls for Hypersonic Flying Vehicle Fuselage / Propulsion

高超声速飞行器/发动机流动控制研究

Simulation on Electro-Hydraulic Proportion Control in Fuselage Lifting System of Glass Tube Cutting Robot

玻璃管切割机器人机身升降电液比例控制系统仿真

Integral Molding on Typical Structure of Composites Forward Fuselage

复合材料前机身典型结构件整体成型

A Study of Application Feasibility of AI-Li Alloy 1441 for Fuselage

对1411铝锂合金作飞机蒙皮的可行性研究

Stability Analysis of Coupled Rotor / Fuselage System with Elastomeric Lag Damper

带粘弹减摆器的旋翼/机体耦合系统稳定性分析

Analysis of Ground Resonance of the Rotor / Fuselage Combind Model Test Stand

旋翼/机身组合模型试验台地面共振分析

Transonic flow field analysis for real fuselage configurations

实际机身跨音速流场分析计算