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      KCI등재 SCIE SCOPUS

      Numerical simulations of nano-particle’s drag forces using DSMC method for various Knudsen numbers

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      https://www.riss.kr/link?id=A108463352

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      다국어 초록 (Multilingual Abstract)

      In this study, high-vacuum flow was analyzed using the direct simulation Monte Carlo (DSMC) method, and various forces acting on fine particles in a high-vacuum flow field were studied. The DSMC method is a Lagrangian method that models the flow as pa...

      In this study, high-vacuum flow was analyzed using the direct simulation Monte Carlo (DSMC) method, and various forces acting on fine particles in a high-vacuum flow field were studied. The DSMC method is a Lagrangian method that models the flow as particles and analyzes the collisions and behaviors of each particle, which costs a large computing resource.
      To validate DSMC method, computational results of a Poiseuille flow in microchannel are compared with analytical results. In addition, the force acting on the particles in the high-vacuum rarefied gas region was verified using the outputs of previous studies. Through this numerical analysis, it is possible to analyze about regions that are difficult to proceed with experiments.
      As a result, the drag forces according to the Knudsen number which indicates the ratio of vacuum and the particle size, it was confirmed that the drag force can be predicted through the empirical formula of previous studies.

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      참고문헌 (Reference) 논문관계도

      1 G. A. Bird, "The velocity distribution function within a shock wave" 30 (30): 479-487, 1967

      2 G. A. Bird, "The structure of rarefied gas flows past simple aerodynamic shapes" 36 (36): 571-, 1969

      3 G. A. Bird, "The structure of normal shock waves in a binary gas mixture" 31 (31): 657-668, 1968

      4 R. A. Millikan, "The isolation of an ion, a precision measurement of its charge, and the correction of stokes’s law" 32 (32): 436-448, 1910

      5 R. A. Millikan, "The general law of fall of a small spherical body through a gas, and its bearing upon the nature of molecular reflection from surfaces" 22 (22): 1-23, 1923

      6 S. Chapman, "The Mathematical Theory of Non-uniform Gases, an Account of the Kinetic Theory of Viscosity, Thermal Conduction and Diffusion of Gases" Cambridge University Press 1952

      7 R. T. Birge, "The 1944 values of certain atomic constants with particular reference to the electronic charge" 13 (13): 63-73, 1945

      8 J. H. Kim, "Slip correction measurements of certified PSL nanoparticles using a nanometer differential mobility analyzer (nano-DMA) for Knudsen number from 05 to 83" 110 (110): 31-, 2005

      9 K. Swaminathan-Gopalan, "Recommended direct simulation Monte Carlo collision model parameters for modeling ionized air transport processes" 28 (28): 027101-, 2016

      10 E. P. Muntz, "Rarefied gas dynamics" 21 : 387-417, 1989

      1 G. A. Bird, "The velocity distribution function within a shock wave" 30 (30): 479-487, 1967

      2 G. A. Bird, "The structure of rarefied gas flows past simple aerodynamic shapes" 36 (36): 571-, 1969

      3 G. A. Bird, "The structure of normal shock waves in a binary gas mixture" 31 (31): 657-668, 1968

      4 R. A. Millikan, "The isolation of an ion, a precision measurement of its charge, and the correction of stokes’s law" 32 (32): 436-448, 1910

      5 R. A. Millikan, "The general law of fall of a small spherical body through a gas, and its bearing upon the nature of molecular reflection from surfaces" 22 (22): 1-23, 1923

      6 S. Chapman, "The Mathematical Theory of Non-uniform Gases, an Account of the Kinetic Theory of Viscosity, Thermal Conduction and Diffusion of Gases" Cambridge University Press 1952

      7 R. T. Birge, "The 1944 values of certain atomic constants with particular reference to the electronic charge" 13 (13): 63-73, 1945

      8 J. H. Kim, "Slip correction measurements of certified PSL nanoparticles using a nanometer differential mobility analyzer (nano-DMA) for Knudsen number from 05 to 83" 110 (110): 31-, 2005

      9 K. Swaminathan-Gopalan, "Recommended direct simulation Monte Carlo collision model parameters for modeling ionized air transport processes" 28 (28): 027101-, 2016

      10 E. P. Muntz, "Rarefied gas dynamics" 21 : 387-417, 1989

      11 G. Russo, "Plane Couette flow computations by TRMC and MFS methods" 762 : 577-, 2005

      12 T. Ozawa, "Particle and continuum method comparison of a high-altitude, extreme-Mach-number reentry flow" 24 (24): 225-240, 2010

      13 E. A. Malkov, "Parallelization of algorithms for solving the Boltzmann equation for GPU-based computations" 1333 : 946-, 2011

      14 H. Burau, "PIConGPU : a fully relativistic particle-in-cell code for a GPU cluster" 38 (38): 2831-2839, 2010

      15 C. Emma, "On the velocity of steady fall of spherical particles through fluid medium" 83 (83): 357-365, 1910

      16 E. S. Piekos, "Numerical modeling of micromechanical devices using the direct simulation Monte Carlo method" 118 (118): 464-469, 1996

      17 G. A. Bird, "Molecular Gas Dynamics and the Direct Simulation of Gas Flows" Clarendon Press 1994

      18 Z. Li, "Modeling of electronic excitation and radiation in non-continuum hypersonic reentry flows" 23 (23): 066102-, 2011

      19 M. Knudsen, "Luftwiderstand gegen die langsame bewegung kleiner kugeln" 341 (341): 981-994, 1911

      20 I. Sohn, "Efficiency enhancement of PIC-MCC modeling for magnetron sputtering simulations using GPU parallelization" 44 (44): 1823-1833, 2016

      21 G. A. Bird, "Direct simulation and the Boltzmann equation" 13 (13): 2676-, 1970

      22 G. A. Bird, "Direct molecular simulation of a dissociating diatomic gas" 25 (25): 353-365, 1977

      23 T. Ozawa, "Development of kineticbased energy exchange models for noncontinuum, ionized hypersonic flows" 20 (20): 046102-, 2008

      24 I. Sohn, "Coupled DSMC-PMC radiation simulations of a hypersonic reentry" 26 (26): 22-35, 2012

      25 G. A. Bird, "Aspects of the structure of strong shock waves" 13 (13): 1172-, 1970

      26 T. E. Schwartzentruber, "A hybrid particlecontinuum method applied to shock waves" 215 (215): 402-416, 2006

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