Gridless DSMC. Spencer Olson. University of Michigan Naval Research Laboratory Now at: Air Force Research Laboratory

Size: px
Start display at page:

Download "Gridless DSMC. Spencer Olson. University of Michigan Naval Research Laboratory Now at: Air Force Research Laboratory"

Transcription

1 Gridless DSMC Spencer Olson University of Michigan Naval Research Laboratory Now at: Air Force Research Laboratory Collaborator: Andrew Christlieb, Michigan State University 8 June June 2009 J Comp Phys, Vol 227, pp , 2008.

2 Outline Background Algorithm Overview Test Cases Low velocity flow Hypersonic flow

3 Gas Dynamics Simulation Approaches Discrete Particle Model Rarefied Dense Inviscid Free-Particle Limit Limit Fig. 1.1, G. A. Bird, Molecular Gas Dynamics and the Direct Simulation of Gas Flows, : Local Knudsen number : Mean free path : Local Characteristic length

4 Continuous Solution? What about a numerical solution of the Boltzmann equation? : Collision integral : N-Body phase-space density For cm/s and ~10µ m X 10µ m X 1mm resolution, need ~>> 1 TB of memory! (and a lifetime to compute the collision integral)

5 Direct Simulation of gas dynamics using Monte Carlo

6 Direct Simulation of gas dynamics using Monte Carlo Grid Truncate collision integral

7 Direct Simulation of gas dynamics using Monte Carlo Grid Ansatz: Collisional processes separable from particle motion. Collide Transport

8 Grid Mismatch: Coarse Grid Grid Density variations could be due to: Shockwaves Nonfree particle systems Transient processes Captures only low-density dynamics well Allows non-probable collisions

9 Grid Mismatch: Fine Grid Grid Density variations could be due to: Shockwaves Nonfree particle systems Transient processes Captures only high-density dynamics well Wastes memory resources Thermally isolates particles that should be allowed to collide

10 Particle Method of Choice: DSMC Direct Simulation of gas dynamics using Monte Carlo (DSMC) Algorithm: Collide Sort (gridless) Update/Sample macroscopic gas quantities Move (integrate) Apply Boundary Conditions (reflections, absorption,etc.)

11 Simple Gridless Case: Binary Sort/Search Algorithm LNOHFMJIDKBA CEG

12 Binary Sort/Search Algorithm NOHFMJIDKBACEG L H N F J M O D G I K B E A C

13 Binary Sort/Search Algorithm IDKBACEG L H N F J M O D G I K B E A C

14 Binary Sort/Search Algorithm CEG L H N F J M O D G I K B E A C

15 Binary Sort/Search Algorithm Execution time: Sort: Search: (averaged over all trees) L H N F J M O D G I K B E A C

16 Binary Sort/Search Algorithm Execution time: Sort: Search: (averaged over all trees) H D L B F J N A C E G I K M O

17 Quadtree Sorting: Divisions about Geometric Center A Divide by geometric center Disallow children with too few particles Avoid bad aspect ratio A B C B C D E F G F G H I H

18 Quadtree Sorting: Divisions about Geometric Center A Divide by geometric center Disallow children with too few particles Avoid bad aspect ratio A B C B C D E F G F G H I H

19 Quadtree Sorting: Divisions about Geometric Center A Divide by geometric center Disallow children with too few particles Avoid bad aspect ratio A B C B C D E F G F G H I H

20 Quadtree Sorting: Divisions about Center of Mass A Divide by center of mass Disallow children with too few particles Avoid bad aspect ratio Shrink to avoid large empty space A B C B C D E F L J F G H I J K L M H

21 Quadtree Sorting Divisions about Geometric Center Large Empty Space Avoided Divisions about Center of Mass Minimal Bounded Volume

22 DSMC Validity Condition : Scale size of nodes : Mean collision separation F. J. Alexander, A.~L. Garcia, B. J. Alder, Cell size dependence of transport coefficients in stochastic particle algorithms, Phys. Fluids, 10: , 1998.

23 DSMC Validity Condition Validity Metric F. J. Alexander, A.~L. Garcia, B. J. Alder, Cell size dependence of transport coefficients in stochastic particle algorithms, Phys. Fluids, 10: , 1998.

24 Quadtree Example

25 Getting the Collision Rate Correct (Grid Based) Time counting methods: In each cycle, evaluate random collision pairs until desired collision rate is met. Collision probability and spacing mismatched in time. Not vectorizable (multi-processor code not easy) G. A. Birds NTC method (1989) Calculate number of tested collisions ahead of time (no time mismatch problems). Vectorizable.

26 Getting the Collision Rate Correct (Grid Based) Grid G. A. Birds NTC method (1989) #Select =

27 Getting the Collision Rate Correct (Tree Based) Grid Gridless ~ --> time averaged gridless data #Select =

28 Move Particles Solve Using favorite integrator. Free particles: RK2, leap-frog, etc. Non-free particles: Adaptive RK5 (embedded RK4 for error detection) RK4 (with small time step) etc.

29 Apply Boundary Conditions 1. Scale boundary boxes 2. Test boundary boxes for overlap with tree nodes 3. Allow each overlapped boundary to interact with tree node particles Each boundary segment treated as an individual object with its own interaction logic

30 Example Boundary (collisional)

31 Test Cases Couette flow Velocity diffusion Thermal diffusion Very low velocity flow past thin plate Hypersonic flow Square cylinder Biconic cylinder (2D) (static shock-shock interaction) Evaporative cooling in ultracold gas

32 Couette Flow Flow between two infinite parallel plates. Case 1: Case 2: 32

33 Couette Flow: v 2 v 1 = 300m/s Gridded DSMC data provided by Dr. Quanhua Sun 33

34 Hypersonic Flow Mach 10 Gas: Argon Compared to results from G. A. Bird's DS2V program Case 1: Square Cylinder Case 2: Biconic Cylinder (2D) 34

35 Hypersonic Flow: Square Cylinder Mach 10 Gas: Argon Compared to results from G. A. Bird's DS2V program Case 1: Square Cylinder 8 m Computational domain Case 2: Biconic Cylinder (2D) v m

36 Hypersonic Flow: Square Cylinder Number Density Gridless DSMC Mach Number DS2V DSMC Temperature 36

37 DSMC Validity Condition: Square Cylinder Validity condition met: Uniform validity throughout. Gridless DSMC Validity condition met: Non-uniform validity metric. Cell size might possibly be made too small causes thermal isolation. DS2V DSMC

38 Hypersonic Flow: Biconic Cylinder (2D) Mach 10 Gas: Argon Compared to results from G. A. Bird's DS2V program Case 1: Square Cylinder 25 cm Computational domain Case 2: Biconic Cylinder (2D) v 20 cm J. N. Moss, G. A. Bird, and G. N. Markelov, DSMC Simulations of Hypersonic Flows and Comparison With Experiments, Rarefied Gas Dynamics: 24 th Intntl. Sym. on Rare. Gas Dyn,

39 DSMC Validity Condition: Biconic Cylinder (2D) Validity condition NOT met: Non-uniform validity metric not enough particles Gridless DSMC Validity condition partially met: Non-uniform validity metric. Cell size may be too small causes thermal isolation. DS2V DSMC

40 DSMC Validity Condition: Biconic Cylinder (2D) Validity condition met: N ~ X13 N 0 Gridless DSMC Validity condition met: Non-uniform validity metric. Cell size may still be too small causes thermal isolation. N ~ X13 N 0 DS2V DSMC

41 Future Work In the middle of a major code-rewrite Faster: Sort time Tree traversal time Handles multiple particle types Arbitrary collision equation sets (only binary input now) Integrate with multipole-expansion treecode field solvers Simulate plasma+neutral shock-shock interactions Continue boundary code development 41

Application of a Modular Particle-Continuum Method to Partially Rarefied, Hypersonic Flows

Application of a Modular Particle-Continuum Method to Partially Rarefied, Hypersonic Flows Application of a Modular Particle-Continuum Method to Partially Rarefied, Hypersonic Flows Timothy R. Deschenes and Iain D. Boyd Department of Aerospace Engineering, University of Michigan, Ann Arbor,

More information

Navier Stokes Solvers. Length (Log meters) Particle Methods. Density (Log n/n 0. Knudsen number =1/10 2. Dense Gas

Navier Stokes Solvers. Length (Log meters) Particle Methods. Density (Log n/n 0. Knudsen number =1/10 2. Dense Gas Mesh and Algorithm Reænement Alejandro L. Garcia Center for Comp. Sciences and Engineering Lawrence Berkeley National Laboratory and Dept. Physics, San Jose State University Collaborators: Berni Alder

More information

Stefan Stefanov Bulgarian Academy of Science, Bulgaria Ali Amiri-Jaghargh Ehsan Roohi Hamid Niazmand Ferdowsi University of Mashhad, Iran

Stefan Stefanov Bulgarian Academy of Science, Bulgaria Ali Amiri-Jaghargh Ehsan Roohi Hamid Niazmand Ferdowsi University of Mashhad, Iran Stefan Stefanov Bulgarian Academy of Science, Bulgaria Ali Amiri-Jaghargh Ehsan Roohi Hamid Niazmand Ferdowsi University of Mashhad, Iran Outlines: Introduction DSMC Collision Schemes Results Conclusion

More information

Application of the Transition Probability Matrix Method to High Knudsen Number Flow Past a Micro-Plate

Application of the Transition Probability Matrix Method to High Knudsen Number Flow Past a Micro-Plate Application of the Transition Probability Matrix Method to High Knudsen Number Flow Past a Micro-Plate Andrew J. Christlieb, W. Nicholas G. Hitchon, Quanhua Sun and Iain D. Boyd Department of Aerospace

More information

Kinetic Models and Gas-Kinetic Schemes with Rotational Degrees of Freedom for Hybrid Continuum/Kinetic Boltzmann Methods

Kinetic Models and Gas-Kinetic Schemes with Rotational Degrees of Freedom for Hybrid Continuum/Kinetic Boltzmann Methods Kinetic Models and Gas-Kinetic Schemes with Rotational Degrees of Freedom for Hybrid Continuum/Kinetic Boltzmann Methods Simone Colonia, René Steijl and George N. Barakos CFD Laboratory - School of Engineering

More information

Omid Ejtehadi Ehsan Roohi, Javad Abolfazli Esfahani. Department of Mechanical Engineering Ferdowsi university of Mashhad, Iran

Omid Ejtehadi Ehsan Roohi, Javad Abolfazli Esfahani. Department of Mechanical Engineering Ferdowsi university of Mashhad, Iran Omid Ejtehadi Ehsan Roohi, Javad Abolfazli Esfahani Department of Mechanical Engineering Ferdowsi university of Mashhad, Iran Overview Micro/Nano Couette Flow DSMC Algorithm Code Validation Entropy and

More information

19 th INTERNATIONAL CONGRESS ON ACOUSTICS MADRID, 2-7 SEPTEMBER 2007

19 th INTERNATIONAL CONGRESS ON ACOUSTICS MADRID, 2-7 SEPTEMBER 2007 19 th INTERNATIONAL CONGRESS ON ACOUSTICS MADRID, -7 SEPTEMBER 007 INVESTIGATION OF AMPLITUDE DEPENDENCE ON NONLINEAR ACOUSTICS USING THE DIRECT SIMULATION MONTE CARLO METHOD PACS: 43.5.Ed Hanford, Amanda

More information

Development of a General Purpose DSMC Flow Solver on Unstructured Meshes. Code

Development of a General Purpose DSMC Flow Solver on Unstructured Meshes. Code 36th AIAA Thermophysics Conference 23-26 June 2003, Orlando, Florida AIAA 2003-3776 Development of a General Purpose DSMC Flow Solver on Unstructured Meshes V. Tenishev,M.Combi Space Physics Research Laboratory,

More information

The deposition efficiency and spatial thickness distribution of films created by Directed

The deposition efficiency and spatial thickness distribution of films created by Directed Chapter 8 Vapor Transport Model Development The deposition efficiency and spatial thickness distribution of films created by Directed Vapor Deposition synthesis have been shown to be sensitive functions

More information

A Hybrid Continuum / Particle Approach for Micro-Scale Gas Flows

A Hybrid Continuum / Particle Approach for Micro-Scale Gas Flows A Hybrid Continuum / Particle Approach for Micro-Scale Gas Flows Quanhua Sun *, Iain D. Boyd * and Graham V. Candler * Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 489 Department

More information

Predicting Breakdown of the Continuum Equations Under Rarefied Flow Conditions

Predicting Breakdown of the Continuum Equations Under Rarefied Flow Conditions Predicting Breakdown of the Continuum Equations Under Rarefied Flow Conditions Iain D. Boyd Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109 Abstract. The breakdown of the

More information

DSMC solver for an optimized Space Crew reentry Orbital Vehicle

DSMC solver for an optimized Space Crew reentry Orbital Vehicle DSMC solver for an optimized Space Crew reentry Orbital Vehicle Vigneshwaran Krishnamurthy 1,a, Ram Arvinth Shanmugam Periasamy 1,b, Vertika Saxena 1,c, Nandita Nurani Hari 1,d and Suriyaprabha Chandrasekar

More information

DSMC Modeling of Rarefied Flow through Micro/Nano Backward-Facing Steps

DSMC Modeling of Rarefied Flow through Micro/Nano Backward-Facing Steps DSMC Modeling of Rarefied Flow through Micro/Nano Backward-Facing Steps Amir-Mehran Mahdavi 1, Ehsan Roohi 2 1,2- Department of Mechanical Engineering, Faculty of Engineering, Ferdowsi university of Mashhad,

More information

Boltzmann Solver with Adaptive Mesh in Phase Space

Boltzmann Solver with Adaptive Mesh in Phase Space Boltzmann Solver with Adaptive Mesh in Phase Space Vladimir Kolobov, Robert Arslanbekov CFD Research Corporation, Huntsville, AL, USA Anna Frolova Dorodnitsyn Computing Center of RAS, Moscow, Russia Topical

More information

Vibrational degrees of freedom in the Total Collision Energy DSMC chemistry model

Vibrational degrees of freedom in the Total Collision Energy DSMC chemistry model Vibrational degrees of freedom in the Total Collision Energy DSMC chemistry model Mark Goldsworthy, Michael Macrossan Centre for Hypersonics, School of Engineering, University of Queensland, Brisbane,

More information

Particle Simulation of Hall Thruster Plumes in the 12V Vacuum Chamber

Particle Simulation of Hall Thruster Plumes in the 12V Vacuum Chamber Particle Simulation of Hall Thruster Plumes in the 12V Vacuum Chamber IEPC-2005-138 Presented at the 29 th International Electric Propulsion Conference, Princeton University, Iain D. Boyd 1, Quanhua Sun

More information

All-Particle Multiscale Computation of Hypersonic Rarefied Flow

All-Particle Multiscale Computation of Hypersonic Rarefied Flow 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 4-7 January 2010, Orlando, Florida AIAA 2010-822 All-Particle Multiscale Computation of Hypersonic Rarefied

More information

VERIFICATION AND VALIDATION OF A PARALLEL 3D DIRECT SIMULATION MONTE CARLO SOLVER FOR ATMOSPHERIC ENTRY APPLICATIONS

VERIFICATION AND VALIDATION OF A PARALLEL 3D DIRECT SIMULATION MONTE CARLO SOLVER FOR ATMOSPHERIC ENTRY APPLICATIONS VERIFICATION AND VALIDATION OF A PARALLEL 3D DIRECT SIMULATION MONTE CARLO SOLVER FOR ATMOSPHERIC ENTRY APPLICATIONS Paul Nizenkov and Stefanos Fasoulas Institut für Raumfahrtsysteme (IRS), Universität

More information

Micro- and nanoscale non-ideal gas Poiseuille flows in a consistent Boltzmann algorithm model

Micro- and nanoscale non-ideal gas Poiseuille flows in a consistent Boltzmann algorithm model INSTITUTE OFPHYSICS PUBLISHING JOURNAL OFMICROMECHANICS ANDMICROENGINEERING J. Micromech. Microeng. () 7 PII: S9-7()7-9 Micro- and nanoscale non-ideal gas Poiseuille flows in a consistent Boltzmann algorithm

More information

TAU Extensions for High Enthalpy Flows. Sebastian Karl AS-RF

TAU Extensions for High Enthalpy Flows. Sebastian Karl AS-RF TAU Extensions for High Enthalpy Flows Sebastian Karl AS-RF Contents Motivation Extensions available in the current release: Numerical schemes for super- and hypersonic flow fields Models for gas mixtures,

More information

Treecodes for Cosmology Thomas Quinn University of Washington N-Body Shop

Treecodes for Cosmology Thomas Quinn University of Washington N-Body Shop Treecodes for Cosmology Thomas Quinn University of Washington N-Body Shop Outline Motivation Multipole Expansions Tree Algorithms Periodic Boundaries Time integration Gravitational Softening SPH Parallel

More information

DIRECT SIMULATION CALCULATIONS OF THE RAREFIED HYPERSONIC FLOW PAST A BACKWARD-FACING STEP

DIRECT SIMULATION CALCULATIONS OF THE RAREFIED HYPERSONIC FLOW PAST A BACKWARD-FACING STEP 9 Brazilian Symposium on Aerospace Eng. & Applications Copyright c 9 by AAB September 14-16, 9, S. J. Campos, SP, Brazil DIRECT SIMULATION CALCULATIONS OF THE RAREFIED HPERSONIC FLOW PAST A BACKWARD-FACING

More information

Scaling Parameters in Rarefied Flow and the Breakdown of the Navier-Stokes Equations Mechanical Engineering Research Report No: 2004/09

Scaling Parameters in Rarefied Flow and the Breakdown of the Navier-Stokes Equations Mechanical Engineering Research Report No: 2004/09 Scaling Parameters in Rarefied Flow and the Breakdown of the Navier-Stokes Equations Mechanical Engineering Research Report No: 2004/09 Michael Macrossan, Centre for Hypersonics, University of Queensland

More information

On the Expedient Solution of the Boltzmann Equation by Modified Time Relaxed Monte Carlo (MTRMC) Method

On the Expedient Solution of the Boltzmann Equation by Modified Time Relaxed Monte Carlo (MTRMC) Method Journal of Applied Fluid Mechanics, Vol. 11, No. 3, pp. 655-666, 2018. Available online at www.jafmonline.net, ISSN 1735-3572, EISSN 1735-3645. DOI: 10.18869/acadpub.jafm.73.246.28007 On the Expedient

More information

Stochastic Particle Methods for Rarefied Gases

Stochastic Particle Methods for Rarefied Gases CCES Seminar WS 2/3 Stochastic Particle Methods for Rarefied Gases Julian Köllermeier RWTH Aachen University Supervisor: Prof. Dr. Manuel Torrilhon Center for Computational Engineering Science Mathematics

More information

HYPERSONIC AERODYNAMICS OF TOROIDAL BALLUTES

HYPERSONIC AERODYNAMICS OF TOROIDAL BALLUTES 7 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES HYPERSONIC AERODYNAMICS OF TOROIDAL BALLUTES Vladimir V. Riabov Rivier College, Nashua, New Hampshire 36, USA Keywords: DSMC method, aerodynamic

More information

Numerical Simulations. Duncan Christie

Numerical Simulations. Duncan Christie Numerical Simulations Duncan Christie Motivation There isn t enough time to derive the necessary methods to do numerical simulations, but there is enough time to survey what methods and codes are available

More information

Overview of Accelerated Simulation Methods for Plasma Kinetics

Overview of Accelerated Simulation Methods for Plasma Kinetics Overview of Accelerated Simulation Methods for Plasma Kinetics R.E. Caflisch 1 In collaboration with: J.L. Cambier 2, B.I. Cohen 3, A.M. Dimits 3, L.F. Ricketson 1,4, M.S. Rosin 1,5, B. Yann 1 1 UCLA Math

More information

Problems of Flows Through Short Channels Studied by Means of the Boltzmann Equation

Problems of Flows Through Short Channels Studied by Means of the Boltzmann Equation Problems of Flows Through Short Channels Studied by Means of the Boltzmann Equation Aristov V.V., Frolova A.A. and Zabelok S.A. Dorodnicyn Computing Centre of Russian Academy of Sciences Kolobov V.I. and

More information

Kinetic Effects in Spherical Expanding Flows of Binary-Gas Mixtures

Kinetic Effects in Spherical Expanding Flows of Binary-Gas Mixtures Kinetic Effects in Spherical Expanding Flows of Binary-Gas Mixtures Vladimir V. Riabov Rivier College, Nashua, New Hampshire, USA Abstract. Diffusion effects in the spherical expanding flows of argon-helium

More information

A Unified Gas-kinetic Scheme for Continuum and Rarefied Flows

A Unified Gas-kinetic Scheme for Continuum and Rarefied Flows A Unified Gas-kinetic Scheme for Continuum and Rarefied Flows K. Xu and J.C. Huang Mathematics Department, Hong Kong University of Science and Technology, Hong Kong Department of Merchant Marine, National

More information

Surprising i Hydrodynamic d Results Discovered by means of Direct Simulation Monte Carlo

Surprising i Hydrodynamic d Results Discovered by means of Direct Simulation Monte Carlo Surprising i Hydrodynamic d Results Discovered by means of Direct Simulation Monte Carlo Alejandro L. Garcia San Jose State University Lawrence Berkeley Nat. Lab. RTO-AVT-VKI Lecture Series, January 24

More information

SIMULATION OF GAS FLOW OVER MICRO-SCALE AIRFOILS USING A HYBRID CONTINUUM-PARTICLE APPROACH

SIMULATION OF GAS FLOW OVER MICRO-SCALE AIRFOILS USING A HYBRID CONTINUUM-PARTICLE APPROACH 33rd AIAA Fluid Dynamics Conference and Exhibit 3-6 June 3, Orlando, Florida AIAA 3-44 33 rd AIAA Fluid Dynamics Conference and Exhibit / Orlando, Florida / 3-6 Jun 3 SIMULATION OF GAS FLOW OVER MICRO-SCALE

More information

Rarefaction Effects in Hypersonic Aerodynamics

Rarefaction Effects in Hypersonic Aerodynamics Rarefaction Effects in Hypersonic Aerodynamics Vladimir V. Riabov Department of Mathematics and Computer Science, Rivier College, 4 S. Main St., Nashua, NH 6, USA Abstract. The Direct Simulation Monte-Carlo

More information

Hypersonic Flow over a Wedge with a Particle Flux Method

Hypersonic Flow over a Wedge with a Particle Flux Method Hypersonic Flow over a Wedge with a Particle Flux Method M. N. Macrossan, M. V. Metchnik and P. A. Pinto Centre for Hypersonics, School of Engineering, University of Queensland, St Lucia, 47, Australia

More information

arxiv: v1 [physics.comp-ph] 12 Nov 2018

arxiv: v1 [physics.comp-ph] 12 Nov 2018 arxiv:1811.04742v1 [physics.comp-ph] 12 Nov 2018 Load balancing strategies for the DSMC simulation of hypersonic flows using HPC T. Binder 1, S. Copplestone 2, A. Mirza 1, P. Nizenkov 1, P. Ortwein 2,

More information

Development of an evaporation boundary condition for DSMC method with application to meteoroid entry

Development of an evaporation boundary condition for DSMC method with application to meteoroid entry Development of an evaporation boundary condition for DSMC method with application to meteoroid entry F. Bariselli, S. Boccelli, A. Frezzotti, A. Hubin, T. Magin Annual METRO meeting 29th November 2016

More information

Gas-Surface Interaction Effect on Round Leading Edge Aerothermodynamics

Gas-Surface Interaction Effect on Round Leading Edge Aerothermodynamics Brazilian Journal of Physics, vol. 37, no. 2A, June, 2007 337 Gas-Surface Interaction Effect on Round Leading Edge Aerothermodynamics Wilson F. N. Santos National Institute for Space Research, Cachoeira

More information

DSMC Collision Model for the Lennard-Jones Potential: Efficient Algorithm and Verification

DSMC Collision Model for the Lennard-Jones Potential: Efficient Algorithm and Verification Purdue University Purdue e-pubs School of Aeronautics and Astronautics Faculty Publications School of Aeronautics and Astronautics 2011 DSMC Collision Model for the Lennard-Jones Potential: Efficient Algorithm

More information

CORBIS: Code Raréfié Bidimensionnel Implicite Stationnaire

CORBIS: Code Raréfié Bidimensionnel Implicite Stationnaire CORBIS: Code Raréfié Bidimensionnel Implicite Stationnaire main ingredients: [LM (M3AS 00, JCP 00)] plane flow: D BGK Model conservative and entropic velocity discretization space discretization: finite

More information

Numerical Green s Function Techniques

Numerical Green s Function Techniques Numerical Green s Function Techniques Andrew J. Christlieb University Department of This work supported by AFOSR and AFRL. Co-Workers Senior Collaborators Iain Boyd (U Mich) Jean-Luc Cambier (AFRL: Edward

More information

Comparison of Numerical Solutions for the Boltzmann Equation and Different Moment Models

Comparison of Numerical Solutions for the Boltzmann Equation and Different Moment Models Comparison of Numerical Solutions for the Boltzmann Equation and Different Moment Models Julian Koellermeier, Manuel Torrilhon October 12th, 2015 Chinese Academy of Sciences, Beijing Julian Koellermeier,

More information

Monte Carlo simulations of dense gas flow and heat transfer in micro- and nano-channels

Monte Carlo simulations of dense gas flow and heat transfer in micro- and nano-channels Science in China Ser. E Engineering & Materials Science 2005 Vol.48 No.3 317 325 317 Monte Carlo simulations of dense gas flow and heat transfer in micro- and nano-channels WANG Moran & LI Zhixin Department

More information

High Altitude Rocket Plume and Thermal Radiation Analysis

High Altitude Rocket Plume and Thermal Radiation Analysis High Altitude Rocket Plume and Thermal Radiation Analysis [ Woo Jin Jeon, Seung Wook Baek, Jae Hyun Park and Dong Sung Ha ] Abstract In this study, rocket plume behavior at various altitudes and radiative

More information

Hypersonic Flow of Rarefied Gas Near the Brazilian Satellite During its Reentry into Atmosphere

Hypersonic Flow of Rarefied Gas Near the Brazilian Satellite During its Reentry into Atmosphere 398 Brazilian Journal of Physics, vol. 33, no. 2, June, 2003 Hypersonic Flow of Rarefied Gas Near the Brazilian Satellite During its Reentry into Atmosphere Felix Sharipov Departamento de Física, Universidade

More information

HYPERSONIC vehicles generate multi-scale gas flows as a result of both large variations in mean-free-path and

HYPERSONIC vehicles generate multi-scale gas flows as a result of both large variations in mean-free-path and 39th AIAA Thermophysics Conference 25-28 June 27, Miami, FL AIAA 27-3892 Hybrid Particle-Continuum Simulations of Low Knudsen Number Hypersonic Flows Thomas E. Schwartzentruber, Leonardo C. Scalabrin and

More information

Subsonic choked flow in the microchannel

Subsonic choked flow in the microchannel PHYSICS OF FLUIDS 18, 127104 2006 Subsonic choked flow in the microchannel Xie Chong a Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics of the Chinese Academy of Sciences, 15 West

More information

Comparison and Analysis of Chemical Models, methodologies and parameters in Hypersonic Rarefied Flows

Comparison and Analysis of Chemical Models, methodologies and parameters in Hypersonic Rarefied Flows University of Naples Federico II Ph.D. thesis Comparison and Analysis of Chemical Models, methodologies and parameters in Hypersonic Rarefied Flows by Luigi Morsa Coordinator: Prof. Antonio Moccia Tutor:

More information

Fluid Equations for Rarefied Gases

Fluid Equations for Rarefied Gases 1 Fluid Equations for Rarefied Gases Jean-Luc Thiffeault Department of Applied Physics and Applied Mathematics Columbia University http://plasma.ap.columbia.edu/~jeanluc 23 March 2001 with E. A. Spiegel

More information

BOLTZMANN KINETIC THEORY FOR INELASTIC MAXWELL MIXTURES

BOLTZMANN KINETIC THEORY FOR INELASTIC MAXWELL MIXTURES BOLTZMANN KINETIC THEORY FOR INELASTIC MAXWELL MIXTURES Vicente Garzó Departamento de Física, Universidad de Extremadura Badajoz, SPAIN Collaborations Antonio Astillero, Universidad de Extremadura José

More information

Atmospheric Entry. Technology, Mathematical Model and Simulation

Atmospheric Entry. Technology, Mathematical Model and Simulation Atmospheric Entry Technology, Mathematical Model and Simulation Julian Köllermeier RWTH Aachen, August 26th 2016 Outline 1. Introduction to Atmospheric Reentry 2. Rarefied Gases: From Science Fiction to

More information

A comparative study of no-time-counter and majorant collision frequency numerical schemes in DSMC

A comparative study of no-time-counter and majorant collision frequency numerical schemes in DSMC Purdue University Purdue e-pubs School of Aeronautics and Astronautics Faculty Publications School of Aeronautics and Astronautics 2012 A comparative study of no-time-counter and majorant collision frequency

More information

DSMC simulations of thermal escape

DSMC simulations of thermal escape DSMC simulations of thermal escape Alexey N. Volkov, R.E. Johnson, O.J. Tucker, J.T. Erwin Materials Science & Engineering University of Virginia, USA Financial support is provided by NASA through Planetary

More information

A Comparative Study Between Cubic and Ellipsoidal Fokker-Planck Kinetic Models

A Comparative Study Between Cubic and Ellipsoidal Fokker-Planck Kinetic Models A Comparative Study Between Cubic and Ellipsoidal Fokker-Planck Kinetic Models Eunji Jun German Aerospace Center (DLR), 3773 Göttingen, Germany M. Hossein Gorji Computational Mathematics and Simulation

More information

Collisional energy transfer modeling in non-equilibrium condensing flows

Collisional energy transfer modeling in non-equilibrium condensing flows Collisional energy transfer modeling in non-equilibrium condensing flows Natalia Gimelshein, Ingrid Wysong and Sergey Gimelshein ERC, Inc, Edwards AFB, CA 93524 Propulsion Directorate, Edwards AFB, CA

More information

Monte Carlo method with negative particles

Monte Carlo method with negative particles Monte Carlo method with negative particles Bokai Yan Joint work with Russel Caflisch Department of Mathematics, UCLA Bokai Yan (UCLA) Monte Carlo method with negative particles 1/ 2 The long range Coulomb

More information

Lattice Boltzmann simulations on heterogeneous CPU-GPU clusters

Lattice Boltzmann simulations on heterogeneous CPU-GPU clusters Lattice Boltzmann simulations on heterogeneous CPU-GPU clusters H. Köstler 2nd International Symposium Computer Simulations on GPU Freudenstadt, 29.05.2013 1 Contents Motivation walberla software concepts

More information

Modeling of the Electric Field in a Hypersonic Rarefied Flow

Modeling of the Electric Field in a Hypersonic Rarefied Flow 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 4-7 January 2010, Orlando, Florida AIAA 2010-635 Modeling of the Electric Field in a Hypersonic Rarefied Flow

More information

Numerical studies of hypersonic binary gas-mixture flows near a sphere

Numerical studies of hypersonic binary gas-mixture flows near a sphere Numerical studies of hypersonic binary gas-mixture flows near a sphere V.V. Riabov Diffusive Effects in Binary Gas-Mixture Flows near a Sphere Diffusion processes have a significant effect on the structure

More information

THE design of hypersonic vehicles requires accurate prediction

THE design of hypersonic vehicles requires accurate prediction JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER Vol. 22, No. 1, January March 2008 Velocity Slip and Temperature Jump in Hypersonic Aerothermodynamics Andrew J. Lofthouse, Leonardo C. Scalabrin, and Iain D.

More information

Shear Force in Radiometric Flows

Shear Force in Radiometric Flows Shear Force in Radiometric Flows Natalia E. Gimelshein, Sergey F. Gimelshein, Andrew D. Ketsdever and Nathaniel P. Selden ERC, Inc, Edwards AFB, CA 93524 University of Colorado at Colorado Springs, Colorado

More information

An improved unified gas-kinetic scheme and the study of shock structures

An improved unified gas-kinetic scheme and the study of shock structures IMA Journal of Applied Mathematics (2011) 76, 698 711 doi:10.1093/imamat/hxr002 Advance Access publication on March 16, 2011 An improved unified gas-kinetic scheme and the study of shock structures KUN

More information

An Asymptotic-Preserving Monte Carlo Method for the Boltzmann Equation

An Asymptotic-Preserving Monte Carlo Method for the Boltzmann Equation An Asymptotic-Preserving Monte Carlo Method for the Boltzmann Equation Wei Ren a, Hong Liu a,, Shi Jin b,c a J C Wu Center for Aerodynamics, School of Aeronautics and Aerospace, Shanghai Jiao Tong University,

More information

Modelling Neutral & Plasma Chemistry with DSMC

Modelling Neutral & Plasma Chemistry with DSMC Modelling Neutral & Plasma Chemistry with DSMC Timothy J. Bartel Sandia National Labs Albuquerque, New Mexico, USA tjbarte@sandia.gov Abstract. The Direct Simulation Monte Carlo (DSMC) method is a powerful

More information

Fluid Equations for Rarefied Gases

Fluid Equations for Rarefied Gases 1 Fluid Equations for Rarefied Gases Jean-Luc Thiffeault Department of Applied Physics and Applied Mathematics Columbia University http://plasma.ap.columbia.edu/~jeanluc 21 May 2001 with E. A. Spiegel

More information

A Framework for Hybrid Parallel Flow Simulations with a Trillion Cells in Complex Geometries

A Framework for Hybrid Parallel Flow Simulations with a Trillion Cells in Complex Geometries A Framework for Hybrid Parallel Flow Simulations with a Trillion Cells in Complex Geometries SC13, November 21 st 2013 Christian Godenschwager, Florian Schornbaum, Martin Bauer, Harald Köstler, Ulrich

More information

Summary We develop an unconditionally stable explicit particle CFD scheme: Boltzmann Particle Hydrodynamics (BPH)

Summary We develop an unconditionally stable explicit particle CFD scheme: Boltzmann Particle Hydrodynamics (BPH) Summary Steps in BPH Space is divided into Cartesian cells Finite number of particles ~10 6-10 7 Particles fly freely between t n and t n+1 Mass, momentum and total energy are conserved Relax into a (LTE)

More information

Numerical Studies of Heat Transfer on Hypersonic Blunt Bodies with Gas Injection

Numerical Studies of Heat Transfer on Hypersonic Blunt Bodies with Gas Injection Paper 130 Civil-Comp Press, 2010 Proceedings of the Seventh International Conference on Engineering Computational Technology, B.H.V. Topping, J.M. Adam, F.J. Pallarés, R. Bru and M.L. Romero, (Editors),

More information

Entropy and irreversibility in gas dynamics. Joint work with T. Bodineau, I. Gallagher and S. Simonella

Entropy and irreversibility in gas dynamics. Joint work with T. Bodineau, I. Gallagher and S. Simonella Entropy and irreversibility in gas dynamics Joint work with T. Bodineau, I. Gallagher and S. Simonella Kinetic description for a gas of hard spheres Hard sphere dynamics The system evolves under the combined

More information

Chapter 1 Direct Modeling for Computational Fluid Dynamics

Chapter 1 Direct Modeling for Computational Fluid Dynamics Chapter 1 Direct Modeling for Computational Fluid Dynamics Computational fluid dynamics (CFD) is a scientific discipline, which aims to capture fluid motion in a discretized space. The description of the

More information

Monte Carlo methods for kinetic equations

Monte Carlo methods for kinetic equations Monte Carlo methods for kinetic equations Lecture 4: Hybrid methods and variance reduction Lorenzo Pareschi Department of Mathematics & CMCS University of Ferrara Italy http://utenti.unife.it/lorenzo.pareschi/

More information

PROGRESS IN PROBABILISTIC MODELLING OF ATOMIC SPONTANEOUS EMISSION PROCESSES IN DSMC

PROGRESS IN PROBABILISTIC MODELLING OF ATOMIC SPONTANEOUS EMISSION PROCESSES IN DSMC PROGRESS IN PROBABILISTIC MODELLING OF ATOMIC SPONTANEOUS EMISSION PROCESSES IN DSMC Dejan Petkow (1), Maria Zaretskaya (1), Alexandre Kling (1), Georg Herdrich (2) (1) Advanced Concepts Team (ACT), ESA-ESTEC,

More information

DSMC Simulation of Entry Vehicle Flowfields Using a Collision-Based Chemical Kinetics Approach

DSMC Simulation of Entry Vehicle Flowfields Using a Collision-Based Chemical Kinetics Approach DSMC Simulation of Entry Vehicle Flowfields Using a Collision-Based Chemical Kinetics Approach R.G. Wilmoth a, D.B. VanGilder a, and J.L. Papp a a Combustion Research and Flow Technology, Inc., 6210 Keller

More information

Planar Laser-Induced Iodine Fluorescence Technique for Flow Visualization and Quantitative Measurements in Rarefied Flows

Planar Laser-Induced Iodine Fluorescence Technique for Flow Visualization and Quantitative Measurements in Rarefied Flows Planar Laser-Induced Iodine Fluorescence Technique for Flow Visualization and Quantitative Measurements in Rarefied Flows Professor James McDaniel*, Eric Cecil*, Erin Reed* and Josh Codoni* Professor Iain

More information

Coupling atomistic and continuum modelling of magnetism

Coupling atomistic and continuum modelling of magnetism Coupling atomistic and continuum modelling of magnetism M. Poluektov 1,2 G. Kreiss 2 O. Eriksson 3 1 University of Warwick WMG International Institute for Nanocomposites Manufacturing 2 Uppsala University

More information

Numerical Simulation of the Rarefied Gas Flow through a Short Channel into a Vacuum

Numerical Simulation of the Rarefied Gas Flow through a Short Channel into a Vacuum Numerical Simulation of the Rarefied Gas Flow through a Short Channel into a Vacuum Oleg Sazhin Ural State University, Lenin av.5, 6283 Ekaterinburg, Russia E-mail: oleg.sazhin@uralmail.com Abstract. The

More information

On the expedient solution of the Boltzmann equation by Modified Time Relaxed Monte Carlo (MTRMC) method

On the expedient solution of the Boltzmann equation by Modified Time Relaxed Monte Carlo (MTRMC) method On the expedient solution of the Boltzmann equation by Modified Time Relaxed Monte Carlo (M) method M. Eskandari 1 and S.S. Nourazar 1 Department of Mechanical Engineering, Amirkabir University of Technology,

More information

Regularization of the Chapman-Enskog Expansion and Its Description of Shock Structure

Regularization of the Chapman-Enskog Expansion and Its Description of Shock Structure NASA/CR-2001-211268 ICASE Report No. 2001-39 Regularization of the Chapman-Enskog Expansion and Its Description of Shock Structure Kun Xu Hong Kong University, Kowloon, Hong Kong ICASE NASA Langley Research

More information

Monte Carlo Simulation of Hypersonic Rarefied Gas Flow using Rotationally and Vibrationally Inelastic Cross Section Models

Monte Carlo Simulation of Hypersonic Rarefied Gas Flow using Rotationally and Vibrationally Inelastic Cross Section Models Monte Carlo Simulation of Hypersonic Rarefied Gas Flow using Rotationally and Vibrationally Inastic Cross Section Mods Hiroaki Matsumoto a a Division of systems research, Yokohama National University 79-5

More information

Direct Simulation of Ultrafast Detonations in Mixtures

Direct Simulation of Ultrafast Detonations in Mixtures Direct Simulation of Ultrafast Detonations in Mixtures Patrick D. O Connor *, Lyle N. Long * and James B. Anderson * Department of Aerospace Engineering, The Pennsylvania State University, University Park,

More information

A discontinuous Galerkin fast spectral method for the multi-species Boltzmann equation

A discontinuous Galerkin fast spectral method for the multi-species Boltzmann equation A discontinuous Galerkin fast spectral method for the multi-species Boltzmann equation Shashank Jaiswal a, Alina A. Alexeenko a, Jingwei Hu b, a School of Aeronautics and Astronautics, Purdue University,

More information

Simulation of the Interaction Between Two Counterflowing Rarefied Jets

Simulation of the Interaction Between Two Counterflowing Rarefied Jets Simulation of the Interaction Between Two Counterflowing Rarefied Jets Cyril Galitzine and Iain D. Boyd Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109 Abstract. A preliminary

More information

Hypersonic Blunt Body Thermophysics Using a Unified Kinetic/Continuum Solver

Hypersonic Blunt Body Thermophysics Using a Unified Kinetic/Continuum Solver 41st AIAA Thermophysics Conference 22-25 June 2009, San Antonio, Texas AIAA 2009-3838 Hypersonic Blunt Body Thermophysics Using a Unified Kinetic/Continuum Solver Andrew J. Lofthouse U.S. Air Force Institute

More information

REGULARIZATION AND BOUNDARY CONDITIONS FOR THE 13 MOMENT EQUATIONS

REGULARIZATION AND BOUNDARY CONDITIONS FOR THE 13 MOMENT EQUATIONS 1 REGULARIZATION AND BOUNDARY CONDITIONS FOR THE 13 MOMENT EQUATIONS HENNING STRUCHTRUP ETH Zürich, Department of Materials, Polymer Physics, CH-8093 Zürich, Switzerland (on leave from University of Victoria,

More information

Numerical Simulation of Microwave Plasma Thruster Flow

Numerical Simulation of Microwave Plasma Thruster Flow Numerical Simulation of Microwave Plasma Thruster Flow IEPC-2007-211 Presented at the 30 th International Electric Propulsion Conference, Florence, Italy September 17-20, 2007 Mao-lin Chen *, Mao Gen-wang,

More information

Numerical Characterization of Multi-Dielectric Green s Function for 3-D Capacitance Extraction with Floating Random Walk Algorithm

Numerical Characterization of Multi-Dielectric Green s Function for 3-D Capacitance Extraction with Floating Random Walk Algorithm Numerical Characterization of Multi-Dielectric Green s Function for 3-D Capacitance Extraction with Floating Random Walk Algorithm Hao Zhuang 1, 2, Wenjian Yu 1 *, Gang Hu 1, Zuochang Ye 3 1 Department

More information

Direct Monte Carlo Simulations of a Binary Gas Free-Jet Flow Over a Flat Plate

Direct Monte Carlo Simulations of a Binary Gas Free-Jet Flow Over a Flat Plate Direct Monte Carlo Simulations of a Binary Gas Free-Jet Flow Over a Flat Plate Eric Cecil Department of Mechanical and Aerospace Engineering, University of Virginia, Charlottesville, VA 2293, USA Abstract.

More information

On the motion induced in a gas confined in a small-scale gap due to instantaneous boundary heating

On the motion induced in a gas confined in a small-scale gap due to instantaneous boundary heating J. Fluid Mech. (7), vol. 593, pp. 453 46. c 7 Cambridge University Press doi:.7/s78658 Printed in the United Kingdom 453 On the motion induced in a gas confined in a small-scale gap due to instantaneous

More information

NUMERICAL SIMULATION OF THE BLAST IMPACT PROBLEM USING THE DIRECT SIMULATION MONTE CARLO (DSMC) METHOD

NUMERICAL SIMULATION OF THE BLAST IMPACT PROBLEM USING THE DIRECT SIMULATION MONTE CARLO (DSMC) METHOD NUMERICAL SIMULATION OF THE BLAST IMPACT PROBLEM USING THE DIRECT SIMULATION MONTE CARLO (DSMC) METHOD Anupam Sharma 1 and Lyle N. Long 2 Department of Aerospace Engineering, 233 Hammond Building University

More information

Failures of the Burnett and super-burnett equations in steady state processes

Failures of the Burnett and super-burnett equations in steady state processes Continuum Mech. Thermodyn. (2005) 7: 43 50 Digital Object Identifier (DOI) 0.007/s006-004-086-0 Original article Failures of the Burnett and super-burnett equations in steady state processes H. Struchtrup

More information

SIMULATION OF COMPRESSIBLE GAS FLOW IN A MICRONOZZLE Effect of Walls on Shock Structure

SIMULATION OF COMPRESSIBLE GAS FLOW IN A MICRONOZZLE Effect of Walls on Shock Structure AIAA - 2001-3073 SIMULATION OF COMPRESSIBLE GAS FLOW IN A MICRONOZZLE Effect of Walls on Shock Structure By M. Buoni, D. Dietz, K. Aslam, and V. V. Subramaniam Center for Advanced Plasma Engineering Non-Equilibrium

More information

Why Should We Be Interested in Hydrodynamics?

Why Should We Be Interested in Hydrodynamics? Why Should We Be Interested in Hydrodynamics? Li-Shi Luo Department of Mathematics and Statistics Center for Computational Sciences Old Dominion University, Norfolk, Virginia 23529, USA Email: lluo@odu.edu

More information

Algorithms PART II: Partitioning and Divide & Conquer. HPC Fall 2007 Prof. Robert van Engelen

Algorithms PART II: Partitioning and Divide & Conquer. HPC Fall 2007 Prof. Robert van Engelen Algorithms PART II: Partitioning and Divide & Conquer HPC Fall 2007 Prof. Robert van Engelen Overview Partitioning strategies Divide and conquer strategies Further reading HPC Fall 2007 2 Partitioning

More information

Problem. Problem Given a dictionary and a word. Which page (if any) contains the given word? 3 / 26

Problem. Problem Given a dictionary and a word. Which page (if any) contains the given word? 3 / 26 Binary Search Introduction Problem Problem Given a dictionary and a word. Which page (if any) contains the given word? 3 / 26 Strategy 1: Random Search Randomly select a page until the page containing

More information

Numerical Simulation of Rarefied-Gas Flows about a Rotating Cylinder

Numerical Simulation of Rarefied-Gas Flows about a Rotating Cylinder Numerical Simulation of Rarefied-Gas Flows about a Rotating Cylinder Vladimir V. Riabov Department of Computer Science, Rivier College, 42 South Main Street, Nashua, NH 36-86, USA Abstract. Subsonic and

More information

ABSTRACT. Nomenclature

ABSTRACT. Nomenclature ABSTRACT The behavior of two different models of gas-surface interactions is studied using the Direct Simulation Monte Carlo (DSMC) method. The DSMC calculations examine differences in predictions of aerodynamic

More information

Computation of Shock Waves in Inert Binary Gas Mixtures in Nonequilibrium Using the Generalized Boltzmann Equation

Computation of Shock Waves in Inert Binary Gas Mixtures in Nonequilibrium Using the Generalized Boltzmann Equation 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 09-12 January 2012, Nashville, Tennessee AIAA 2012-0361 Computation of Shock Waves in Inert Binary Gas Mixtures

More information

Ultra-Cold Plasma: Ion Motion

Ultra-Cold Plasma: Ion Motion Ultra-Cold Plasma: Ion Motion F. Robicheaux Physics Department, Auburn University Collaborator: James D. Hanson This work supported by the DOE. Discussion w/ experimentalists: Rolston, Roberts, Killian,

More information

Simplified Hyperbolic Moment Equations

Simplified Hyperbolic Moment Equations Simplified Hyperbolic Moment Equations Julian Koellermeier and Manuel Torrilhon Abstract Hyperbolicity is a necessary property of model equations for the solution of the BGK equation to achieve stable

More information

A Hybrid CFD-DSMC Method of Modeling Continuum-Rarefied Flows

A Hybrid CFD-DSMC Method of Modeling Continuum-Rarefied Flows 42nd AIAA Aerospace Sciences Meeting and Exhibit 5-8 January 24, Reno, Nevada AIAA 24-8 42nd AIAA Aerospace Sciences Meeting and Exhibit Reno, NV January 5 8, 24 A - Method of Modeling Continuum-Rarefied

More information