声速的

Air-breathing hypersonic vehicle has been the next generation single stage to orbit vehicle and hypersonic cruise vehicle.

吸气式高超声速飞行器是下一代单级入轨和高超声速巡航研究的重点飞行器。

For the radiation transfer equation, both the spatial domain and the angular domain is discretized, and the finite volume method is used to solve the equation in an explicit way.

把一种新的三维热辐射计算方法应用到高超声速非平衡流场的数值模拟过程中：在非结构网格上对高超声速化学非平衡流场的数值模拟过程中，耦合了辐射输运方程来求解辐射热流。

Thus it was extensively applied to experimental research of transonic and hypersonic flow.

因此，它在跨声速和超声速流的实验研究中得以广泛地应用。

Research advances and development of hypersonic vehicles in recent years were reviewed, and relevant technologies of hyersonic vehicles were summarized in this paper firstly.

首先回顾了近年来国外高超声速飞行器的研究现状和进展，对高超声速飞行器的一些相关技术进行了总结。

The Anton Paar Density and Sound Velocity Analyzers combine two independent parameters, density and sound velocity, to cover a wide range of applications such as quality control in beer and soft drink production, concentration determination of sulphuric acid and oleum or ternary solutions.

安东帕密度和声速分析仪结合两种独立参数--密度和声速，覆盖大范围的应用如：啤酒和软饮料生产中的质量管理、硫酸、发烟硫酸或三元混合液体浓度的测定。

Infrared radiation features of water jet were extracted in two and three dimensional configuration.

现代高压水射流技术的喷嘴直径一般在2mm以下，最小可达到0.2mm左右，流速为高亚声速至高超声速。

The simulation results show that there are many factors to influence the reverberation, each of them has different contribution to the reverberation, and the angles configurations and the characters of interface have main function, and the effect of the change of sound velocity on reverberation can be ignored.

模型仿真结果表明，影响双基地声纳混响的因素众多，每个因素在对双基地混响的贡献是不一样的，双基地角度的配置和界面性质变化对混响的影响很大，而声速的变化对混响的影响可以忽略不计。

Firstly, studies for hypersonic inlets are reviewed, including issues related to interaction between boundary and shock wave in hypersonic inlet, unstarting/restarting phenomena, isolator, boundary bleeding for hypersonic inlet, internal/external compression ratio for inlet, inlets with sidewall compression, etc..

首先是高超声速进气道的研究进展，包括高超声速进气道中激波与附面层干扰、起动和再起动、隔离段、进气道附面层抽吸、进气道通道内外压缩比、侧压式进气道、Busemann进气道等。

The structure of supersonic combustion flow field was analyzed. The effects of temperature and equivalent ratio of supersonic premixed flow on the structure of supersonic combustion flow field, ignition and flame propagation were studied.

采用普通的纹影系统实现了高温超声速燃烧流场显示；对超声速燃烧流场结构作出了分析；研究了超声速预混可燃气的温度以及当量比对超声速燃烧流场结构、点火与火焰传播特性的影响。

This paper will systematically expatiate the interrelation and interaction between the factors of sound velocity, instrument correction and index etc.

结合黄骅港水深测量数据，针对声速剖面测量与声速改正以及声速、器差、指标差等要素间的内在联系及相互影响予以系统阐述。

The split between the two groups can hardly be papered over.

这两个团体间的分歧难以掩饰。

This approach not only encourages a greater number of responses, but minimizes the likelihood of stale groupthink.

这种做法不仅鼓励了更多的反应，而且减少跟风的可能性。