飞行器设计

多学科飞行器设计中的FLUENT集成方法研究

Study on FLUENT Integration in Multidisciplinary Flight Vehicle Design

分析了当前多学科飞行器设计中对于商业设计软件集成的需求，提出了基于文件包装器的组件化策略。

In this paper , we begin with an analysis of the demands of integrating heterogeneous commercial off-the-shelf products in multidisciplinary flight vehicle design , and the difficulties are proposed .

采用CFD的方法对这种流动及气动特性进行分析在飞行器设计中具有重要的意义。

It is of importance in aircraft design to analyze this flow and aerodynamic characteristics by means of CFD .

论文共分七章，内容涉及CAD／CAM、飞行器设计、计算几何、计算机图形学等。既有理论研究、方法探讨、又有实际应用。

The dissertation consists of seven chapters which are dealt with many fields , such as CAD / CAM , Aircraft Design , Computational Geometry , Computer Graphics etc.

雷达散射截面（RCS）已成为飞行器设计的一个重要战技指标。

As the flight performance , radar cross section ( RCS ) has become an important tactical and technical target in aircraft designs .

多学科设计优化（Multidisciplinarydesignoptimization，MDO）方法研究耦合多学科系统的设计最优化问题，对于提高飞行器设计水平具有非常现实与重要的意义。

The MDO ( Multidisciplinary Design Optimization ) method handles the optimal design problem of coupled multidisciplinary system . It has very practical and important meaning to increase the aerospace vehicle design level .

对MDO过程理论与先进飞行器设计应用做了大量探索性的工作，为进一步开展飞行器MDO奠定了良好的基础。

Much exploring work of MDO process theory and advanced aerospace design application are done , which establishes a good base for aerospace vehicle MDO .

本文主要针对我国串联两级重复使用跨大气层飞行器设计方案，建立其动力学虚拟样机，并使用该样机对串联两级RLV的上升段进行仿真计算。

The thesis aims at setting up the dynamic virtual prototype for contacting series two stages of RLV system and simulating flight at ascent stage .

学生的成绩将由课堂表现、读书笔记、作业、上交的个人设计文件集和LTA飞行器设计项目这几部分来评定。

Performance will be evaluated on the basis of class participation , reading summaries , problem sets , personal design portfolio submissions , and the LTA vehicle design project .

每年利用搜集到的有关「比空气轻（LTA）」飞行器设计读物和其他讯息，学生须完成小组项目∶制作和竞飞软式小型飞机。

Each year , using readings and other information gathered about " Lighter Than Air "( LTA ) design , the students build and race blimps as a small group project .

面向先进飞行器设计的非定常空气动力学揭示飞行的奥秘推动飞机的发展&空气动力学发展漫谈

UNSTEADY AERODYNAMICS FOR ADVANCED AIRCRAFT DESIGN Gossip About Development of Aerodynamics

快速控制在某种飞行器设计中的应用

An application of the high speed control in some vehicle design

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 .

气动与隐身性能计算精度对飞行器设计的影响

Influence of Aerodynamic and Stealth Performance Computation Precision on Aircraft Optimization Design

每个飞行器设计为可以重复使用一百次。

Each orbiter was designed to be reused up to 100 times .

飞行器设计并行工程中多视图响应分析

Analysis of Multi-view Response in Aircraft Design and Concurrent Engineering

现代飞行器设计中的隐身理念探析

Analysis of Concealed Body Principle in the Modern Aircraft Design

利用这种方法，为再入飞行器设计了自动驾驶仪。

The design process is simpler than others and easy for implement .

前体设计是吸气式高超声速飞行器设计的关键之一。

The forebody design is a key issue for hypersonic airbreathing vehicle .

再入飞行器设计中热环境参数估算方法的探讨

A Study of Estimation Methods of Heat Environment Parameters in Reentry Vehicle Design

最优鲁棒控制在飞行器设计中的应用

The application of optimal robust control in control system design of flying vehicles

计算气动弹性在飞行器设计中的研究与应用

Research and Application of Computational Aero-Elasticity in Aircraft Design

折叠翼是一种很有前景的变体飞行器设计方案。

A strong candidate for morphing wing design is the folding wing configuration .

一种分布式高性能的飞行器设计优化框架面向服务的分布式工作流执行站点优化

A Distributed High-performance Aircraft MDO Framework Execution station optimization for service-oriented distributed workflow

飞行器设计方法在日益激烈的空天竞争中占据重要地位。

Aerospace vehicle design method plays an important role in increasingly intensive aerospace competition .

算例表明算法在飞行器设计中有效。

The calculation example shows that the new algorithm works effectively in aircraft design .

最后还为我国的亚轨道飞行器设计提出了一些可行的操控和制导方案。

The feasible control and guiding scheme of the sub-orbital vehicle are introduced finally .

滑跃式高超音速巡航飞行器设计初步研究

Preliminary design for soaring hypersonic cruise vehicle

另外，对发射场、飞行器设计与控制等方面也进行了详细的方案探讨和初步设计。

Also , the launch pad , space vehicle design and control methodology were discussed .

本文提出的方法对类似飞行器设计具有参考意义。

The methods used in this thesis can be referred by similar aircraft controller design .