英语释义

1. a branch of dynamics that deals with gaseous fluids including products of combustion and plasmas

片语

thermal gasdynamic laser热气动激光器

gasdynamic nonuniformity气体动力非均匀性

gasdynamic functions气动函数

gasdynamic heating气动加热

gasdynamic mode气动模

gasdynamic laser[激光] 气动激光器

gasdynamic effect气体动力效应

hypersonic gasdynamic charts极音速气体动力图表

gasdynamic focus气体动力学焦点

英汉例句

• a model of this type has been designed, which scale is 1∶2. experiments of flow visualization, gasdynamic performance and foreign object throwing have been done.

  针对某型发展型飞机设计并制造了缩尺比例为1∶2的该型式进气道模型，进行了流态观察，气动性能试验和投掷外来物试验。

• the present article deals with the problem of supersonic flow past bodies by a medium with gasdynamic and physicochemical nonuniformities and the effect on the aerodynamic characteristics of bodies.

  本文研究的问题是超声速气流流过物体时产生的气体动力和物理化学非均匀性及其对物体空气动力特性的影响。

• a two-phase base bleed gasdynamic model is presented.

  本文提出了一个新的两相流底排气体动力学模型。

• this paper deals with the gasdynamic process of the spherical piston in a weak field of gravitation.

  本文研究在弱引力场中活塞球对称运动的气体动力学过程。

• recently the shock tube has been used to drive gasdynamic laser.

  最近，激波管已被用来驱动气动激光器。

• in addition, it is indicated that the usage of any transient techniques, numerical as well as experimental, must be careful in evaluation of gasdynamic heating and heat-transfer process.

  同时指出，任何瞬态算法和技术在评估飞行器持续受热和导热问题时必须十分慎重。

• then, rigid body dynamic model and gasdynamic model of air-driven spherical shell were established.

  结果定质量流量供气的气动壳体结构的中性浮力平衡是不稳定的。

• gasdynamic equations of stream-line coordinates which are suitable for the numerical solutions of the two-dimensional subsonic and transonic flows are derived in this paper.

  本文导出了适用于亚、跨音速二维绕流问题数字解的流线座标系气体动力学方程组。

• recent derivations of varying specific heat gasdynamic functions by the author give powerful tool of solving the problem.

  变比热气动函数式的推导，提出了解此问题的有力工具。

• this paper describes a combustion-driven co2 gasdynamic laser with a throat height of 0.3mm and an area-ratio 30 grid nozzles, and presents some experimental results.

  本文介绍了喷管喉道高度为0.3毫米、面积比为30的燃烧驱动co_2气动激光器的某些实验结果。

• influences of the various factors are presented on the jet gasdynamic gains.

  给出了来流马赫数、喷流动量比、喷口布局等对增益特性的影响。