Aerodynamic Configuration

Development and analysis in aerodynamic configuration of cruise missile

巡航导弹气动布局的发展和分析

Some Problems on Aerodynamic Configuration for the Single Rotor Helicopter

单旋翼式直升机气动布局的几个问题

MATLAB-based modern optimal algorithm applied to aerodynamic configuration design of vehicles

基于MATLAB的现代优化算法在飞行器气动外形设计中的应用

An integrated analysis of aerodynamic configuration and control system in design of BTT Missile

BTT导弹总体设计中气动特性与控制系统的协调分析

Aerodynamic Configuration Study of Cable-Stayed Casing Based on the Purpose of Damping

基于减振目的的斜拉索套管气动外形研究

General design of regulating valve system includes aerodynamic configuration design , driven structure design and control system design .

该风洞调压阀总体设计分为调压阀气动外形设计、驱动形式设计及控制系统设计，本论文给出了每个分系统的详细设计过程。

Multiobjective optimization design of aerodynamic configuration constrained by stealth performance

隐身性能约束的多目标气动外形优化设计

Optimization design of aerodynamic configuration for hypersonic cruise vehicle based on ant colony algorithm

基于蚁群算法的高超声速飞行器气动布局优化设计

Flow mechanism investigation for ' W ' tailless aerodynamic configuration

‘W’型无尾布局流动机理研究

Trends in the Development of Aerodynamic Configuration of Guided Weapons and Relevant Aerodynamic Techniques

制导兵器气动布局发展趋势及有关气动力技术

Aerodynamic Configuration Analysis and Engineering Evaluation of the Aerodynamic Characteristics for TW-1 Tow Target

TW－1拖靶外形布局分析和气动力特性估算

It is very difficult to implement high quality only depending upon the stucture design or aerodynamic configuration .

单纯依靠结构设计、气动布局已难实现高品质的要求。

Aerodynamic Configuration Design and Trajectory Simulation of an Interceptor Controlled by Aerodynamic / Lateral Thrust

气动力/直接力复合控制拦截弹的气动外形设计及弹道仿真

Study of Aerodynamic Configuration Design for Buoyancy-lifting Vehicle in Near-space

临近空间浮升一体化飞行器气动布局研究

Computational Study on an Aerodynamic Configuration for SSTO Vehicles

单级入轨运载器气动布局研究

Chapter 1 is the introduction , discussing CFD , non-structural grid method and development of aerodynamic configuration optimization .

引言是第一章，讨论CFD、非结构网格方法及气动外形优化设计方法的发展。

Impacts of Aerodynamic Configuration Parameters on Stabilities of Joined-Wing Aircraft

某联接翼飞机外形参数变化对稳定性影响的研究

This procedure has played an active role in aerodynamic configuration design and characteristics calculation for aircraft B , C , D.

在复杂外形的气动布局设计和气动特性预估中，发挥了积极的作用。

Three structure blueprints based the existent aerodynamic configuration and wing configuration of DF-2 light sports aircraft .

在DF-2轻型体育运动飞机复合材料机翼现有气动外形和机翼布局方案的基础上，设计选用了三种结构方案。

A Preliminary Study on Aircraft Conformal Fuel Tanks in Aerodynamic Configuration Design Aerodynamic performances of several typical designs are analyzed .

飞机保形油箱气动力设计初探对目前国外典型保形油箱的设计方案及气动特性进行了初步的分析。

Flow Mechanism of the Influence of Forward-Swept Angle on the Longitudinal Characteristics of Aerodynamic Configuration with Forward-Swept Wing

机翼掠角对前掠翼布局气动性能影响的流动机理

Aerodynamic configuration design for a parameterized lifting body common aero vehicle Design and Implement of Real-time Virtual Atmosphere Environment Server Based on HLA

通用大气飞行器的参数化气动布局研究无人飞行器飞行实时大气环境仿真服务器

However , owing to the special aerodynamic configuration , the static trimming characteristics cannot entirely meet the criterion for flying qualities .

稳态配平特性主要受构型的影响，飞翼布局飞机一般不能完全满足飞行品质的要求。

Combinatory Optimization of the Vehicle Handling and Stability ; The Aerodynamic Configuration Design of Stability and Control of Canard Configuration Guided Rocket

汽车操纵性与运动稳定性的联合优化设计鸭式制导火箭弹的稳定性与操纵性气动设计

In the flutter model design , dynamical features , stiffness distribution , mass distribution and aerodynamic configuration of real aircraft are needed to be simulated .

颤振模型设计需要模拟真实飞机的动力学特性、刚度分布、质量分布与气动外形。

Based upon the knowledge discussed above , with the multi-subject optimization method , the optimization design system of integration of aerodynamic configuration and stealth is built up .

在以上研究的基础上，利用多学科优化方法，建立了亚、超音速和RCS一体化优化设计的方法。

The paper introduces aerodynamic configuration optimization design of lower Reynold number aeroplane using genetic algorithm , and makes prototypes to test feasibility and correctness of design .

试验结果表明该优化设计方法是十分有效的，可以用来对具有正常布局形式的飞机进行气动外形的优化设计。

It is hypersonic developing direction that ride wave body aerodynamic configuration , dual-mode scramjet and BTT ( bank to turn ) control scheme .

得出采用乘波体气动布局、双模态超燃冲压发动机以及BTT转弯控制是高超音速飞行器适合的发展方向。

The MATLAB based modern optimization algorithms , including genetic algorithm , simulated annealing algorithm and Pareto genetic algorithm , are developed and applied to aerodynamic configuration optimization for hypersonic vehicles .

本文发展了MATLAB语言环境下的现代优化算法，包括遗传算法、模拟退火算法和基于分支联赛选择的多目标遗传算法，并用来求解高超声速飞行器气动外形参数优化问题。

Firstly , the thesis designed the system project , aerodynamic configuration , nub and actuator driving device ; selected actuator , decelerator , feedback system and central controller .

论文首先进行了系统方案、气动力布局、舵面及舵传动装置设计，对舵机、减速器、反馈系统及中央控制器进行了选型；