tailless configuration

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

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。

In this paper are presented the major wind tunnel test results for the direction control of 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。

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

前掠翼融合体无尾布局流动控制技术

Flow mechanism investigation for 'W' tailless aerodynamic configuration

‘W’型无尾布局流动机理研究

Investigation of the direction control for the tailless aircraft configuration

无尾飞机布局方向控制特性研究

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

本文研究大展弦比无尾布局的气动舵面设计问题。

This paper investigates a new flow control technique based on a forward-swept wing blended body ( FBB) tailless configuration by a wind tunnel.

通过风洞实验，研究了基于前掠翼融合体无尾气动布局的一种新概念流动控制技术。

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;

翼身融合飞机（Blended Wing Body Aircraft-BWB Aircraft）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。