tailless的例句大全

Analysis of Wingtip Stalling for Tailless Aircraft

无尾飞机翼尖失速问题研究

A short-haired tailless breed of cat believed to originate on the Isle of Man.

被认为是原产于马恩岛的一种短毛无尾猫。

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。

Uncertain Tailless Aircraft Robust Gain-scheduling Controller Design Using LMI

基于LMI的不确定性无尾飞行器鲁棒变增益控制器设计

Design Robust Mixed-Sensitivity Controller to Uncertain Tailless Aircraft

不确定性无尾飞行器混合灵敏度鲁棒控制器设计

Design of LPV Gain-Scheduling Controller to Uncertain Tailless Aircraft

不确定性无尾飞行器LPV变增益控制器设计

In this paper a tailless aircraft was used as a model. Its dynamics was derived and the state-feedback controller was designed.

以无尾飞行器为例，推导了其动力学模型，并设计了状态反馈控制器。

Over the last seven decades, they've been a proving ground for developments including delta wings, tailless aircraft, and supersonic flight.

在过去的70年，他们已经为包括三角翼，无尾飞机发展的试验场，和超音速飞行。

The dynamic simulation results indicate that the smart skin studied in the paper is able to maintain a sufficient authority to control the tailless aircraft in a low-rate maneuvering.

仿真结果表明，所讨论的智能蒙皮对机动要求不大的无尾飞行器具有足够的控制能力。

Characteristics of tailless aircraft wingtip stalling, including common and unique characteristics compared with other configurations, are analyzed with emphasis placed on the effect of wingtip stalling on flying qualities of tailless aircraft.

首先分析了无尾飞机翼尖失速的特点，包括与其他布局形式共有的和自身特有的特点，重点是翼尖失速对无尾飞机飞行品质的影响。

Aircraft designers routinely use scale models, and in the case of the X-36 Tailless Fighter Agility Research Aircraft, that's as big as it got.

飞机设计师经常使用比例模型，并在案件的X-36战斗机敏捷性研究无尾飞机，这是因为大的，因为它得到了。

Investigation of the direction control for the tailless aircraft configuration

无尾飞机布局方向控制特性研究

Adaptive Control for the Vertical Tailless Aircraft with Thrust Vectoring Control

无垂尾推力矢量飞机的自适应控制仿真研究

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。

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

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。

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。

Flow mechanism investigation for 'W' tailless aerodynamic configuration

‘W’型无尾布局流动机理研究

one of the more notable features of the x-4 bantam, built by northrop, was its semi-tailless design.

对在X-4更突出的特点班特姆由诺斯罗普建成，一，是它的半尾巴设计。

The general conceptual design method of tailless Unmanned Aerial Vehicle ( UAV ) was researched in this paper.

本论文主要研究无尾式 无人机 总体概念性设计方法.