Asset Details
MbrlCatalogueTitleDetail
Do you wish to reserve the book?
CFD Modelling of Flow Characteristics in Micro Shock Tubes
by
Adair, D.
, Jaeger, M.
, Mukhambetiyar, A.
in
Boundary conditions
/ Compressible flow
/ Computational fluid dynamics
/ Computer applications
/ Contact pressure
/ Diaphragm
/ Drug delivery
/ Elastic waves
/ Flow characteristics
/ Fluid dynamics
/ Fluid flow
/ High pressure
/ Hydrodynamics
/ K-epsilon turbulence model
/ Low pressure gases
/ Mathematical models
/ MUSCL schemes
/ Pressure
/ Propulsion systems
/ Rarefaction
/ Rupture
/ Rupturing
/ Shock
/ Shock tubes
/ Shock waves
/ Slip
/ Temperature requirements
/ Turbulence models
/ Unsteady flow
2017
Hey, we have placed the reservation for you!
By the way, why not check out events that you can attend while you pick your title.
You are currently in the queue to collect this book. You will be notified once it is your turn to collect the book.
Oops! Something went wrong.
Looks like we were not able to place the reservation. Kindly try again later.
Are you sure you want to remove the book from the shelf?
CFD Modelling of Flow Characteristics in Micro Shock Tubes
by
Adair, D.
, Jaeger, M.
, Mukhambetiyar, A.
in
Boundary conditions
/ Compressible flow
/ Computational fluid dynamics
/ Computer applications
/ Contact pressure
/ Diaphragm
/ Drug delivery
/ Elastic waves
/ Flow characteristics
/ Fluid dynamics
/ Fluid flow
/ High pressure
/ Hydrodynamics
/ K-epsilon turbulence model
/ Low pressure gases
/ Mathematical models
/ MUSCL schemes
/ Pressure
/ Propulsion systems
/ Rarefaction
/ Rupture
/ Rupturing
/ Shock
/ Shock tubes
/ Shock waves
/ Slip
/ Temperature requirements
/ Turbulence models
/ Unsteady flow
2017
Oops! Something went wrong.
While trying to remove the title from your shelf something went wrong :( Kindly try again later!
Do you wish to request the book?
CFD Modelling of Flow Characteristics in Micro Shock Tubes
by
Adair, D.
, Jaeger, M.
, Mukhambetiyar, A.
in
Boundary conditions
/ Compressible flow
/ Computational fluid dynamics
/ Computer applications
/ Contact pressure
/ Diaphragm
/ Drug delivery
/ Elastic waves
/ Flow characteristics
/ Fluid dynamics
/ Fluid flow
/ High pressure
/ Hydrodynamics
/ K-epsilon turbulence model
/ Low pressure gases
/ Mathematical models
/ MUSCL schemes
/ Pressure
/ Propulsion systems
/ Rarefaction
/ Rupture
/ Rupturing
/ Shock
/ Shock tubes
/ Shock waves
/ Slip
/ Temperature requirements
/ Turbulence models
/ Unsteady flow
2017
Please be aware that the book you have requested cannot be checked out. If you would like to checkout this book, you can reserve another copy
We have requested the book for you!
Your request is successful and it will be processed during the Library working hours. Please check the status of your request in My Requests.
Oops! Something went wrong.
Looks like we were not able to place your request. Kindly try again later.
CFD Modelling of Flow Characteristics in Micro Shock Tubes
Journal Article
CFD Modelling of Flow Characteristics in Micro Shock Tubes
2017
Request Book From Autostore
and Choose the Collection Method
Overview
The use of micro shock tubes has become common in many instruments requiring a high velocity and temperature flow field, for example in micro-propulsion systems and drug delivery devices for medical systems. A shock tube has closed ends, and the flow is generated by the rupture of a diaphragm separating a driver gas at high pressure from a driven gas at relatively low pressure. The rupture results in the movement of a shock wave and contact discontinuity into the low-pressure gas, and an expansion wave into the high pressure gas. The characteristics of the resulting unsteady flow for micro shock tubes are not well known as the physics of such tubes includes additional phenomena such as rarefaction and complex viscous effects at low Reynolds numbers. In the present study, computational fluid dynamics (CFD) calculations are made for unsteady compressible flow within a micro shock tube using the van-Leer MUSCL scheme and the two-layer k-ε turbulence model. Novel results have been obtained and discussed of the effects of using different diaphragm pressure ratios, shock tube diameters and wall boundary conditions, namely no slip and slip walls.
Publisher
Isfahan University of Technology
Subject
This website uses cookies to ensure you get the best experience on our website.