涵道尾桨

基于动量源方法的涵道尾桨CFD分析

CFD Analysis for the Ducted Tail Rotor Based on Momentum-Source Method

前飞状态涵道尾桨气动特性CFD分析

CFD Analysis for the Ducted Tail Rotor in Forward Flight

涵道尾桨的CFD模拟与验证带附体潜艇尾流场的数值模拟与验证

CFD Simulation and Validation of Ducted Tail Rotor Numerical Simulation and Validation of Wake Field of Submarine with Stern Appendage

本文采用CFD方法分析了悬停状态下涵道尾桨的流场特性。

The flow field characteristic of a helicopter ducted tail rotor in hovering were analyzed using CFD method in this paper .

采用CFD（计算流体力学）方法分析在悬停和侧飞时直升机涵道尾桨的流场与性能。

The flow field and performance of a helicopter ducted tail rotor in hovering and sideward flight were analyzed using CFD ( Computational Fluid Dynamic ) technique .

本文建立了一套通过求解湍流Navier-Stokes方程并结合动量源模型，来分析涵道尾桨流场和气动特性的方法。

In this thesis , a numerical simulation method is established by solving the turbulent Navier-Stokes equations coupled with the momentum source model .

直升机悬停时涵道尾桨的需用功率计算

A Method for Predicting Ducted Tail Rotor Power Required in Hovering Flight

直升机涵道尾桨与孤立尾桨的气动特性对比研究

Comparison and Analysis of Aerodynamic characteristics between Helicopter Shrouded and Isolated Tail Rotors