We use a direct simulation Monte Carlo (DSMC) method to simulate gas heating/cooling and choked subsonic flows in micro/nanoscale channels subject to either constant wall temperature or constant/variable heat flux boundary conditions. We show the effects of applying various boundary conditions on the mass flow rate and the flow parameters. We also show that it is necessary to add a buffer zone at the end of the channel if we wish to simulate more realistic conditions at the channel outlet. We also discuss why applying equilibrium-based Maxwellian distribution on molecules coming from the channel outlet, where the flow is nonequilibrium, will not disturb the DSMC solution. The current velocity, pressure, and mass flow rate results are compared with different analytical solutions of the Navier–Stokes equations. Although there are good agreements between the DSMC results and the analytical solutions in low compressible flow, the analytical solutions yield incorrect velocity and mass flow rate values in short micro/nanochannel flows with high compressibility and/or choked flow conditions.
Skip Nav Destination
e-mail: darbandi@sharif.edu
Article navigation
September 2009
This article was originally published in
Journal of Heat Transfer
Research Papers
Direct Simulation Monte Carlo Solution of Subsonic Flow Through Micro/Nanoscale Channels
Ehsan Roohi,
Ehsan Roohi
Department of Aerospace Engineering,
Sharif University of Technology
, P.O. Box 11365-8639, Tehran 11365, Iran
Search for other works by this author on:
Masoud Darbandi,
Masoud Darbandi
Department of Aerospace Engineering,
e-mail: darbandi@sharif.edu
Sharif University of Technology
, P.O. Box 11365-8639, Tehran 11365, Iran
Search for other works by this author on:
Vahid Mirjalili
Vahid Mirjalili
Department of Aerospace Engineering,
Sharif University of Technology
, P.O. Box 11365-8639, Tehran 11365, Iran
Search for other works by this author on:
Ehsan Roohi
Department of Aerospace Engineering,
Sharif University of Technology
, P.O. Box 11365-8639, Tehran 11365, Iran
Masoud Darbandi
Department of Aerospace Engineering,
Sharif University of Technology
, P.O. Box 11365-8639, Tehran 11365, Irane-mail: darbandi@sharif.edu
Vahid Mirjalili
Department of Aerospace Engineering,
Sharif University of Technology
, P.O. Box 11365-8639, Tehran 11365, IranJ. Heat Transfer. Sep 2009, 131(9): 092402 (8 pages)
Published Online: June 24, 2009
Article history
Received:
July 4, 2008
Revised:
April 2, 2009
Published:
June 24, 2009
Citation
Roohi, E., Darbandi, M., and Mirjalili, V. (June 24, 2009). "Direct Simulation Monte Carlo Solution of Subsonic Flow Through Micro/Nanoscale Channels." ASME. J. Heat Transfer. September 2009; 131(9): 092402. https://doi.org/10.1115/1.3139105
Download citation file:
Get Email Alerts
Cited By
Related Articles
A Numerical Method for Turbomachinery Aeroelasticity
J. Turbomach (April,2004)
DSMC Analysis of Rarefied Gas Flow Over a Rectangular Cylinder at All Knudsen Numbers
J. Fluids Eng (December,2000)
Simulation of Compressible Micro-Scale Jet Impingement Heat Transfer
J. Heat Transfer (June,2003)
DSMC Simulation: Validation and Application to Low Speed Gas Flows in Microchannels
J. Fluids Eng (January,2009)
Related Chapters
Natural Gas Transmission
Pipeline Design & Construction: A Practical Approach, Third Edition
Compressive Deformation of Hot-Applied Rubberized Asphalt Waterproofing
Roofing Research and Standards Development: 10th Volume
Fluid Flow Applications
Introduction to Finite Element, Boundary Element, and Meshless Methods: With Applications to Heat Transfer and Fluid Flow