通过核磁共振技术探究固液界面甲醇重整反应

来源 :第二十届全国波谱学学术年会 | 被引量 : 0次 | 上传用户:zhang5658
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
其他文献
Due to the high speed of the supersonic flow in the scramjet combustor,the residence time of fuel remains only a few milliseconds.
A computational scheme of fluidic was conducted which utilizes coflowing and countercurrent shear layers to control thrust vector in the absence of moving parts.
In the development of hypersonic vehicles,a spiked-nose may promote the reduction of shockinduced drag and the decrease of heat flux over blunt bodies.
At supercritical conditions a porous strip(or slot strip)placed beneath a shock wave can reduce the drag by a weaker lambda shock system,and increase the buffet boundary,even may increase the lift.
In this paper,flow and acoustic measurements results of an experimental investigation of supersonic jets exhausting from 30° and 60° beveled nozzles will be presented and discussed.
Shock tubes are devices which are used in the investigation of high speed and high temperature flow of compressible gas.Inside a shock tube,the interaction between the reflected shock wave and boundar
Open-loop active control of bursting process and drag reduction in wall turbulence is realized by utilizing synchronous and asynchronous vibration of double piezoelectric vibrators placed along the sp
As an incident shock passes through an inhomogeneous elliptic gas cylinder,complex wave patterns is formed.
The interaction between a shock wave and a boundary layer along a duct wall forms very complicated flow structures characterized by shock train.
Boltzmann equation based on gas kinetic theory has been well accepted as a more general formulation of gas flows,than Navier-Stokes equation.However,the high computational cost rendered solving Boltzm