说明:双击或选中下面任意单词,将显示该词的音标、读音、翻译等;选中中文或多个词,将显示翻译。
您的位置:首页 -> 句库 -> 旋翼/机身耦合
1.
Aeroelastic Response Analysis of a Coupled Rotor/Fuselage Helicopter System (Ⅰ) Modeling of the Rotary Wing System
直升机旋翼/机身耦合系统的气弹响应分析(一)旋翼系统的建模
2.
The aeromechanical st ability for the coupled rotor/fuselage system of helicopters in forward flight i s investigated.
研究了前飞状态下直升机旋翼 /机身耦合系统的气动 /机械稳定性问题。
3.
Calculation of the Aerodynamic Interaction between Rotor/Wing/Fuselage of Tilt-Rotor;
倾转旋翼飞行器旋翼/机翼/机身气动干扰计算
4.
fuselage-wing-tail combination configuration
机身-机翼-尾翼组合体
5.
The Study of Induced Velocity Field and the Initial Trajectory of the Missile on the Condition of Coupled Rotor/Airframe Helicopter;
旋翼/机体耦合情况下的诱导速度场及对导弹初始弹道研究
6.
Semi-active Control Research about the Dynamic Stability of Rotor/airframe Coupled Basing on Magneto-rheological Damper;
基于磁流变阻尼器的旋翼/机体耦合动稳定性半主动控制研究
7.
Research on Fluid Characteristic within the Rotating-wing Machinery Based on Fluid Structure Interaction Model;
基于流固耦合的小型旋翼式机械内部水流特性的研究
8.
Within this analytical model, the factors as unsteady aerodynamic and blade flap/lead-lag coupled motion are both considered.
旋翼/机体耦合动力学模型考虑了非定常空气动力和桨叶挥舞/摆振运动耦合。
9.
stowed rotor vehicle
旋翼收藏式组合直升机
10.
Influence of wing location on rotor-wing interaction of compound helicopter
机翼位置对复合式直升机旋翼-机翼干扰的影响
11.
wing-to-fuselage fairing
机翼机身接合整流带
12.
Multi body dynamic differential equations are combined with the equations of the unsteady dynamic inflow model to establish the complete unsteadily aeroelastic coupling analytical model of the tiltrotor.
结合动力人流,研究了直升机模式下倾转旋翼机非线性非定常气弹耦合动力学特性。
13.
Neural Network Model of Aerodynamic Interaction Effects of Rotor Wake on Fuselage for Helicopter
旋翼/机身气动干扰的神经网络模型
14.
Rotor-wing interaction analysis of a compound helicopter in forward flight
复合式直升机前飞状态旋翼-机翼干扰计算分析
15.
Numerical Simulation and Analysis of Helicopter Rotor/Fuselage Flowfield Based on CFD Method;
基于CFD方法的直升机旋翼/机身流场模拟及分析
16.
Dynamics of joggling principle for scroll profiles of scroll compressor
涡旋压缩机型线耦合机理动态性研究
17.
Research for Aerodynamic Characteristic of Rotor and Fuselage in Hovering Ground-effect
悬停状态地面效应对旋翼和机身气动特性影响
18.
Bird Impact on Aircraft Leading Edge Simulation with SPH and FEM Coupling Method
SPH和FEM耦合方法分析机翼前缘鸟撞的响应问题