• 不 限
  • 期刊论文
  • 硕博论文
  • 会议论文
  • 报 纸
  • 英文论文
  2. 您的位置
  3. 首页
  4. 会议论文
  5. Interaction of cylindrically converging shock with a double-layer interface

Interaction of cylindrically converging shock with a double-layer interface

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：qiushuicai
【摘 要】
：
When an interface separating two fluids of different properties is impulsively impacted by a shock wave,the perturbations at the interface will grow with time,which is referred to as Richtmyer-Meshkov
【作 者】
：
Fan Lei Juchun Ding Xisheng Luo Ting Si 
【机 构】
：
Advanced Propulsion Laboratory,Department of Modern Mechanics University of Science and Technology o
【出 处】
：
第14届亚洲显示会议(The 14th Asian Symposium on Visualization)
【发表日期】
：
2017年11期
【关键词】
：
Richtmyer-Meshkov instability converging shock wave double-layer interface 
下载到本地 , 更方便阅读
下载此文 赞助VIP
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
　　When an interface separating two fluids of different properties is impulsively impacted by a shock wave,the perturbations at the interface will grow with time,which is referred to as Richtmyer-Meshkov(RM)instability.
其他文献
Thrust Vector Control Using Co-and Counter-Flows
A computational scheme of fluidic was conducted which utilizes coflowing and countercurrent shear layers to control thrust vector in the absence of moving parts.
会议
Fluidic thrust vector controlThrust vector angleShock waveBoundary layer sepa
High Temperature Ablation Test of Graphite Rod using a Small Arc-heated plasma testing facility
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.
会议
plasma testing facilitygraphite ablation
Passive Shock Wave/Boundary Layer Control of Wing at Transonic Speeds
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.
会议
WingShock wave/boundary layer interactionBumpDrag reductionTransonicOptimiz
An Experimental Investigation on Supersonic Jets Issuing from Beveled Nozzles
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.
会议
Supersonic jet noisebeveled nozzleshock wave
A Study on Characteristics of Shock Train inside a Shock Tube
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
会议
Shock TubeReflected Shock WaveBoundary Layer SeparationContact SurfaceShock
Active Control of a Turbulent Boundary Layer by Double Piezoelectric Vibrators
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
会议
turbulent boundary layeractive controldouble piezoelectric vibratorsdrag redu
On the Interaction of Planar Incident Shock with a Heavy Elliptic Gas Cylinder
As an incident shock passes through an inhomogeneous elliptic gas cylinder,complex wave patterns is formed.
会议
Shock wavegas cylinderRichtmyer-Meshkov instability
Numerical Study on Flow Separation of Shock Train in a Planar Rectangular Duct
The interaction between a shock wave and a boundary layer along a duct wall forms very complicated flow structures characterized by shock train.
会议
shock trainshock boundary layer interactionflow confinementnumerical simulati
Numerical Simulation of Boltzmann Equation for Gas Flows with Dynamic Discrete Ordinate Method
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
会议
Boltzmann equationBGK collision modelMaxwell equilibrium distributionDiscrete
通过核磁共振技术探究固液界面甲醇重整反应
会议