无尾布局

‘W’型无尾布局流动机理研究

Flow mechanism investigation for ' W ' tailless aerodynamic configuration

基于NS方程数值模拟方法，研究了‘W’型无尾布局的流动机理。

The flow mechanism of ' W ' tailless configuration has been investigated by numerical method based on N-S equations in this paper .

翼身融合飞机（BlendedWingBodyAircraft-BWBAircraft）是一种新型高升阻比无尾布局的大型运输机，其气动特性的研究是BWB布局飞机克服众多技术难题的基础。

Blended-Wing-Body ( BWB ) aircraft is a tailless large transport with high lift-drag ratio , and the aerodynamic study for BWB aircraft is a basis of overcoming the technology challenges about it . Firstly , research history on BWB configuration is presented in this paper ;

研究解决无尾布局横航向稳定性的气动力措施。

To study the way to settle the yawing and rolling stability .

前掠翼融合体无尾布局流动控制技术

Flow Control Technique for Forward-swept Wing Blended Body Tailless Configuration

本文研究大展弦比无尾布局的气动舵面设计问题。

The paper investigates aerodynamic design of the control devices for a high aspect ratio tailless configuration .

无尾飞机布局方向控制特性研究

Investigation of the direction control for the tailless aircraft configuration

介绍了无尾飞机布局方向控制特性风洞试验研究的主要结果。

In this paper are presented the major wind tunnel test results for the direction control of the tailless aircraft configuration .

同时分析了无尾飞翼气动布局的主要问题及其解决途径，设计思想符合航空飞行器设计规律。

This design thought conforms to the design rule of aviation craft .