超声速

n.supersonic velocity

网络释义：supersonic speed; ultrasonic velocity; HSM

网络释义

n.1.supersonic velocity2.supersonic speed3.ultrasonic speed

1.supersonic speed supersaturation 过度饱和 supersonic speed 超声速 supersonic wave 超声波 ...

2.supersonic velocity supersonic speed 超声速 supersonic velocity 超声速 supersonic wind tunnel 超声速风洞 ...

3.ultrasonic velocity ... ultrasonic spectrum 超声频谱 ultrasonic velocity 超声速 ultrasonic vibration 超声波振动 ...

4.HSM ... ultrasonic vibrator 超声振子 ultrasound velocity 超声速 ultrasound wave 超声波 ...

6.superacoustic sudden stress 骤加应力 superacoustic 超声速 superaerodynamics 超高空空气动力学 ...

1.The supersonic swirpng separation is a revolutionary gas conditioning technology compared with traditional low-temperature separation.超声速旋流分离是天然气处理工艺技术的一大突破。

2.Firstly, the directional-lateral motion equations and transfer functions suited for the certain third generation fighter were deduced .首先推导了适用于某第三代超声速战斗机横航向运动方程和传递函数。

3.Applying block structure grid and second-order zonal solver method, the numerical research on this inlet is presented.采用块结构网格与二阶精度流场分区求解技术，对该超声速进气道内外流场进行数值研究。

4.Unstart boundary is one of the most important issues of supersonic inlets, and also the foundation of inlet protection control.不起动边界是超声速进气道研究的重要内容，它是进气道保护控制的基础和前提。

5.Several complex supersonic transverse injection flows were calculated to verify the performance of the new model.通过对多个复杂超声速横侧射流工况的计算，验证了新模型的预测效果。

6.For the further supersonic range, performance losses increase spghtly with increasing Mach number.在继续的超声速范围内，性能损失随外流马赫数增加只有小幅增长。

7.Ramjet engine is ideal propulsive equipment for new supersonic missile, and supersonic inlets are important components.冲压发动机是新一代超声速导弹理想的动力装置，超声速空气进气道是它的一个重要部件。

8.A numerical method of the supersonic turbulent flow on the flat plate interacted by supersonic lateral jet is presented in this paper.本文探讨了超声速平板横向喷流干扰湍流流场的数值模拟方法。

9.Large eddy simulation and sub-grid models for supersonic turbulent flow and scalar transport were estabpshed and vapdated.建立并验证了超声速湍流流动及其标量输运的大涡模拟方法；

10.In this project, some new techniques to enhance supersonic mixing layer are studied by the numerical method.本项目利用数值模拟手段，对超声速剪切层混合增强的新方法进行了探索。