高超音速飞行器

近空间高超音速飞行器射频通信黑障研究

Study on Blackout in Near Space Hypersonic Vehicle Radio Frequency Communication

高超音速飞行器是二十一世纪世界航空航天领域发展的重点，是继隐身技术之后军事领域内最重要的进展。

It is very important to develop the hypersonic vehicle in aeronautic and astronautic in 21st century . The hypersonic vehicle is the most important progress following with stealth technology in military domain .

用于高超音速飞行器的涡扇-冲压双循环发动机设计研究

Design Study of a dual-cycle turbofan-ramjet engine for a hypersonic aircraft

超音速/高超音速飞行器湍流流场气动光学效应分析

Numerical Analysis of Aero-optic Effects Induced by the Turbulence Flow Field Surrounding Super / Hypersonic

未来战争中的高超音速飞行器

Hypersonic Vehicles in the Future Warfare

高超音速飞行器发展中的关键技术

Key Technologies in Developing Hypersonic Vehicles

高超音速飞行器及其发展趋势分析

Development Trend of High-Supersonic Vehicle

高超音速飞行器对动力系统-燃料提出了严格的要求。

As the hypersonic flight comes ture , the power system of aerocraft-fuel will face severe request .

高超音速飞行器的动力装置&超音速燃烧冲压发动机的研究已成为当前各军事强国研究的热点。

The scramjet , which is the propulsion of hypersonic vehicle , has become the focus in many military developed countries .

特别值得注意的是在发展超音速和高超音速飞行器的过程中，偏离了莱特理想的工作方式。

Departures form the ideal practice followed by the Wright have been particularly noticeable in the development of supersonic and hypersonic vehicles .

除可作溶剂外，十氢萘还可作为高超音速飞行器最佳的脱氢、裂解吸热燃料以及作为汽车用燃料电池最佳的贮氢媒体。

Besides , decalin can be used as the best endothermal fuel of dehydrogenation and cracking in ramjet and as a hydrogen source for fuel-cell vehicle .

高超音速飞行器具有凭借其高速度（巡航马赫数6&10），在不超过10分钟的时间内就能够打击近千公里远的目标。

Hypersonic aircraft can attack the goal nearly one thousand kilometers far during the time under 10 minutes relying on high speed ( cruise at 6-10 Mach ) .

根据高超音速飞行器的特点，设计了高超音速飞行器的任务剖面，包括初始段、巡航段和末端攻击段。

2 , According to the characteristic of the hypersonic aircraft , the task of designing the hypersonic aircraft include initial phase , cruise phase and end attack phase .

利用碳氢燃料的物理和化学热沉对高超音速飞行器的发动机等高温部件进行冷却是目前最可行的方法。

The cooling technology using the physical and chemical heat sink of hydrocarbon fuel provides the best means for the thermal management of engine system and the body of advanced aircraft .

而冲压发动机不需转动的叶轮机械，结构简单，高速性能优良，被广泛用于各类超音速和高超音速飞行器，愈来愈受到人们的关注。

Ramjet has been widely used in all kinds of supersonic and high-supersonic aircraft . It has caught more and more attention recently because there is no need for rotating impeller machine .

航空燃料的临界温度和临界压力数据是燃料性能评价的重要参数，直接影响着燃料在未来的航天飞机及高超音速飞行器中的使用状态及应用范围。

Critical temperatures and pressures of fuels are important parameters for rating of merit , which define the phase behaviors , performance and temperature range of fuels applied in the airplanes and hypersonic aircrafts .

正确预测飞行器表面的摩阻和热参数对于高超音速飞行器的成功设计是至关重要的，而这又取决于边界层转捩位置的正确预测。

For a successful design of hypersonic flying vehicles , the correct prediction of the skin friction and heat condition is essential , which in turn depends on the correct prediction of the transition location of the boundary layer .

对滑跃式高超音速巡航飞行器的动力技术进行了初步研究，分析了采用火箭基组合循环发动机（RBCC）方案所需的燃料消耗。

Finally dynamic technology of soaring hypersonic cruise vehicle was preliminarily investigated . The fuel consumption of rocket based combined cycle ( RBCC ) for the soaring hypersonic cruise vehicle was analyzed .

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

在分析国外滑跃式高超音速巡航飞行器的发展现状基础上，提出了高超音速巡航飞行器的概念设计，对滑跃式高超音速巡航飞行器总体方案提出了设想。

On the basis of analyzing development status of soaring hypersonic cruise vehicle abroad , the conceptual design of hypersonic cruise vehicle was put forward , and system scheme of soaring hypersonic cruise vehicle was given .

高超音速BTT巡航飞行器变结构控制系统设计

Design of Variable Structure Control System for Hypersonic BTT Vehicle