The susceptible measurement of low Pitot pressure in shock tunnel

来源 :第14届亚洲显示会议(The 14th Asian Symposium on Visualization) | 被引量 : 0次 | 上传用户:quyeliang
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
  In hypervelocity flows the speed of the considered fluid is much larger than the speed of sound.
其他文献
This paper presents the results of controlling of the laminar separation effectively and eliminates or decreases the nonlinearities of the lift curve.
Recently,various studies of Micro Air Vehicle(MAV)and Unmanned Air Vehicle(UAV)have been reported from wide range points of view [1].
Energy harvesting from vortex-induced vibration(ⅤⅣ)is increasingly concerned recently in applications of wind energy.
There are all kinds of compression corners in the flow path of the hypersonic crafts.
The prediction of skin friction is an important part for hypersonic fluid dynamics,while it is a hard problem for both wind tunnel experiments and numerical simulations.
Deflected beam visualization(such as Schlieren and shadowgraph technique)is usually used to detect the flow structure in hypersonic flow.
When a sonic or supersonic jet is injected laterally into supersonic or hypersonic free stream,the complex jet interactive flowfields is generated which involves highly complicated flow phenomena such
The schlieren system plays an important role in the visualization of hypersonic flow fields.
Some obstacles mounted on the vehicles are unavoidable problems. It is very popular and important for engineering design.
The cylindrical converging shock reflection over a curved wedge is investigated experimentally in a converging shock tube.