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air bubble is disappear increasing time using vof |
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January 15, 2008, 07:25 |
air bubble is disappear increasing time using vof
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#1 |
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i will try using your method. recently, i simulated a single bubble of quiescent water in a closed tank using vof model, however, i found the volume fraction of bubble is decreasing with increasing time, the interface of bubble is blurry,even to disappear, my mesh is very good and the number of the meshes in a bubble is about 20, i think the mesh is very enough, i do not know how to do ? anyone give me suggestion,thanks in advance. this is out file:
| | CFX Command Language for Run | | | +--------------------------------------------------------------------+ EXECUTION CONTROL: RUN DEFINITION: Definition File = D:/xjj/2mmbubble_009.res Interpolate Initial Values = Off Run Mode = Full END PARALLEL HOST LIBRARY: HOST DEFINITION: b Installation Root = C:\CFXb\CFX-%v Host Architecture String = intel_pentium_winnt5.1 END END PARTITIONER STEP CONTROL: Multidomain Option = Independent Partitioning Runtime Priority = Standard MEMORY CONTROL: Memory Allocation Factor = 1.0 END PARTITIONING TYPE: MeTiS Type = k-way Option = MeTiS Partition Size Rule = Automatic Partition Weight Factors = 0.500, 0.500 END END SOLVER STEP CONTROL: Runtime Priority = Standard EXECUTABLE SELECTION: Double Precision = Off END MEMORY CONTROL: Memory Allocation Factor = 1.0 END PARALLEL ENVIRONMENT: Number of Processes = 2 Start Method = PVM Local Parallel Parallel Host List = b*2 END END END LIBRARY: CEL: EXPRESSIONS: DenH = 1000 [kg m^-3] DownH1 = 0.048 [m] Rbubble1 = 0.001 [m] dist1 = Rbubble1-sqrt((x-0.0025[m])^2+(z-0.002[m])^2) UpVFbubble1 = step((dist1)/1[m]) UpVFwater1 = 1-UpVFbubble1 Pres1 = DenH*g*UpVFwater1*DownH1 END END MATERIAL: Air at 25 C Material Description = Air at 25 C and 1 atm (dry) Material Group = Air Data, Constant Property Gases Option = Pure Substance Thermodynamic State = Gas PROPERTIES: Option = General Material Thermal Expansivity = 0.003356 [K^-1] ABSORPTION COEFFICIENT: Absorption Coefficient = 0.01 [m^-1] Option = Value END DYNAMIC VISCOSITY: Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1] Option = Value END EQUATION OF STATE: Density = 1.185 [kg m^-3] Molar Mass = 28.96 [kg kmol^-1] Option = Value END REFRACTIVE INDEX: Option = Value Refractive Index = 1.0 [m m^-1] END SCATTERING COEFFICIENT: Option = Value Scattering Coefficient = 0.0 [m^-1] END SPECIFIC HEAT CAPACITY: Option = Value Reference Pressure = 1 [atm] Reference Specific Enthalpy = 0. [J/kg] Reference Specific Entropy = 0. [J/kg/K] Reference Temperature = 25 [C] Specific Heat Capacity = 1.0044E+03 [J kg^-1 K^-1] Specific Heat Type = Constant Pressure END THERMAL CONDUCTIVITY: Option = Value Thermal Conductivity = 2.61E-02 [W m^-1 K^-1] END END END MATERIAL: Water Material Description = Water (liquid) Material Group = Water Data, Constant Property Liquids Option = Pure Substance Thermodynamic State = Liquid PROPERTIES: Option = General Material Thermal Expansivity = 2.57E-04 [K^-1] ABSORPTION COEFFICIENT: Absorption Coefficient = 1.0 [m^-1] Option = Value END DYNAMIC VISCOSITY: Dynamic Viscosity = 8.899E-4 [kg m^-1 s^-1] Option = Value END EQUATION OF STATE: Density = 997.0 [kg m^-3] Molar Mass = 18.02 [kg kmol^-1] Option = Value END REFRACTIVE INDEX: Option = Value Refractive Index = 1.0 [m m^-1] END SCATTERING COEFFICIENT: Option = Value Scattering Coefficient = 0.0 [m^-1] END SPECIFIC HEAT CAPACITY: Option = Value Reference Pressure = 1 [atm] Reference Specific Enthalpy = 0.0 [J/kg] Reference Specific Entropy = 0.0 [J/kg/K] Reference Temperature = 25 [C] Specific Heat Capacity = 4181.7 [J kg^-1 K^-1] Specific Heat Type = Constant Pressure END THERMAL CONDUCTIVITY: Option = Value Thermal Conductivity = 0.6069 [W m^-1 K^-1] END END END END FLOW: DOMAIN: Domain 1 Coord Frame = Coord 0 Domain Type = Fluid Fluids List = Air at 25 C,Water Location = Assembly BOUNDARY: out Boundary Type = OPENING Location = OUTLET BOUNDARY CONDITIONS: FLOW DIRECTION: Option = Normal to Boundary Condition END FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Option = Opening Pressure and Direction Relative Pressure = 0 [Pa] END END FLUID: Air at 25 C BOUNDARY CONDITIONS: VOLUME FRACTION: Option = Value Volume Fraction = 1 END END END FLUID: Water BOUNDARY CONDITIONS: VOLUME FRACTION: Option = Value Volume Fraction = 0 END END END END BOUNDARY: Domain 1 Default Boundary Type = WALL Location = INLET,SURFS A,SURFS B BOUNDARY CONDITIONS: WALL INFLUENCE ON FLOW: Option = No Slip END END FLUID PAIR: Air at 25 C | Water BOUNDARY CONDITIONS: WALL ADHESION: Option = None END END END END BOUNDARY: sym1 Boundary Type = SYMMETRY Location = FRONT END BOUNDARY: sym2 Boundary Type = SYMMETRY Location = BACK END DOMAIN MODELS: BUOYANCY MODEL: Buoyancy Reference Density = 1.3 [kg m^-3] Gravity X Component = 0 [m s^-2] Gravity Y Component = 0 [m s^-2] Gravity Z Component = -9.8 [m s^-2] Option = Buoyant BUOYANCY REFERENCE LOCATION: Option = Automatic END END DOMAIN MOTION: Option = Stationary END MESH DEFORMATION: Option = None END REFERENCE PRESSURE: Reference Pressure = 1 [atm] END END FLUID: Air at 25 C FLUID MODELS: FLUID BUOYANCY MODEL: Option = Density Difference END MORPHOLOGY: Option = Continuous Fluid END END END FLUID: Water FLUID MODELS: FLUID BUOYANCY MODEL: Option = Density Difference END MORPHOLOGY: Option = Continuous Fluid END END END FLUID MODELS: COMBUSTION MODEL: Option = None END HEAT TRANSFER MODEL: Fluid Temperature = 25 [C] Homogeneous Model = True Option = Isothermal END THERMAL RADIATION MODEL: Option = None END TURBULENCE MODEL: Option = Laminar END END FLUID PAIR: Air at 25 C | Water Surface Tension Coefficient = 0.07256 [N m^-1] INTERPHASE TRANSFER MODEL: Option = Free Surface END MASS TRANSFER: Option = None END SURFACE TENSION MODEL: Option = Continuum Surface Force Primary Fluid = Air at 25 C Volume Fraction Smoothing Type = Volume-Weighted END END MULTIPHASE MODELS: Homogeneous Model = On FREE SURFACE MODEL: Option = Standard END END END INITIALISATION: Option = Automatic FLUID: Air at 25 C INITIAL CONDITIONS: VOLUME FRACTION: Option = Automatic with Value Volume Fraction = UpVFbubble1 END END END FLUID: Water INITIAL CONDITIONS: VOLUME FRACTION: Option = Automatic with Value Volume Fraction = UpVFwater1 END END END INITIAL CONDITIONS: Velocity Type = Cartesian CARTESIAN VELOCITY COMPONENTS: Option = Automatic with Value U = 0 [m s^-1] V = 0 [m s^-1] W = 0 [m s^-1] END STATIC PRESSURE: Option = Automatic with Value Relative Pressure = Pres1 END END END OUTPUT CONTROL: RESULTS: File Compression Level = Default Option = Standard END TRANSIENT RESULTS: Transient Results 1 File Compression Level = Default Option = Standard Time Interval = 0.002 [s] END END SIMULATION TYPE: Option = Transient INITIAL TIME: Option = Automatic with Value Time = 0 [s] END TIME DURATION: Option = Total Time Total Time = 1 [s] END TIME STEPS: Option = Timesteps Timesteps = 0.0001 [s] END END SOLUTION UNITS: Angle Units = [rad] Length Units = [m] Mass Units = [kg] Solid Angle Units = [sr] Temperature Units = [K] Time Units = [s] END SOLVER CONTROL: ADVECTION SCHEME: Option = High Resolution END CONVERGENCE CONTROL: Maximum Number of Coefficient Loops = 15 Timescale Control = Coefficient Loops END CONVERGENCE CRITERIA: Residual Target = 0.00001 Residual Type = RMS END TRANSIENT SCHEME: Option = Second Order Backward Euler END END END COMMAND FILE: Version = 10.0 Results Version = 10.0 END +--------------------------------------------------------------------+ | | | Partitioning | | | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | | | ANSYS CFX Partitioner 10.0 | | | | Version 2005.07.11-10.24 Mon Jul 11 10:26:04 GMTDT 2005 | | | | Executable Attributes | | | | single-32bit-optimised-supfort-noprof-nospag-lcomp | | | | Copyright 1996-2005 ANSYS Europe Ltd. | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Job Information | +--------------------------------------------------------------------+ Run mode: partitioning run Host computer: B Job started: Thu Jan 10 10:18:41 2008 +--------------------------------------------------------------------+ | Memory Allocated for Run (Actual usage may be less) | +--------------------------------------------------------------------+ Data Type Kwords Words/Node Words/Elem Kbytes Bytes/Node Real 2120.0 13.25 26.80 8281.2 53.00 Integer 6895.9 43.10 87.18 26937.0 172.40 Character 1997.4 12.48 25.25 1950.6 12.48 Logical 40.0 0.25 0.51 156.2 1.00 Double 949.7 5.94 12.01 7419.6 47.49 +--------------------------------------------------------------------+ | Total Number of Nodes, Elements, and Faces | +--------------------------------------------------------------------+ Domain Name : Domain 1 Total Number of Nodes = 160000 Total Number of Elements = 79101 Total Number of Hexahedrons = 79101 Total Number of Faces = 159998 +--------------------------------------------------------------------+ | Partitioning Information | +--------------------------------------------------------------------+ Partitioning of domain: Domain 1 - Partitioning tool: MeTiS multilevel weighted k-way algorithm - Number of partitions: 2 - Number of graph-nodes: 160000 - Number of graph-edges: 796400 Partitioning information for domain: Domain 1 +-----------+---------------------+-----------+--------+ | Elements | Vertices (Overlap) | Faces | Weight | +-------------+-----------+---------------------+-----------+--------+ | Full mesh | 79101 | 160000 | 159998 | | +-------------+-----------+---------------------+-----------+--------+ | Part. 1 | 39631 | 80274 0.3% | 80155 | 0.500 | | Part. 2 | 39587 | 80198 0.3% | 80079 | 0.500 | +-------------+-----------+---------------------+-----------+--------+ | Sum of part.| 79218 | 160472 0.3% | 160234 | 1.000 | +-------------+-----------+---------------------+-----------+--------+ CPU-Time requirements: - Preparations 1.406E-01 seconds - Low-level mesh partitioning 9.375E-02 seconds - Global partitioning information 3.125E-02 seconds - Vertex, element and face partitioning information 9.375E-02 seconds - Element and face set partitioning information 4.688E-02 seconds - Summed CPU-time for mesh partitioning 9.219E-01 seconds +--------------------------------------------------------------------+ | Job Information | +--------------------------------------------------------------------+ Host computer: B Job finished: Thu Jan 10 10:18:44 2008 Total CPU time: 1.516E+00 seconds or: ( 0: 0: 0: 1.516 ) ( Days: Hours: Minutes: Seconds ) Total wall clock time: 3.000E+00 seconds or: ( 0: 0: 0: 3.000 ) ( Days: Hours: Minutes: Seconds ) +--------------------------------------------------------------------+ | | | Solver | | | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | | | ANSYS CFX Solver 10.0 | | | | Version 2005.07.11-10.24 Mon Jul 11 10:26:04 GMTDT 2005 | | | | Executable Attributes | | | | single-32bit-optimised-supfort-noprof-nospag-lcomp | | | | Copyright 1996-2005 ANSYS Europe Ltd. | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Job Information | +--------------------------------------------------------------------+ Run mode: parallel run (PVM) Host computer: B Par. Process: Master running on mesh partition: 1 Job started: Thu Jan 10 10:18:45 2008 Host computer: B Par. Process: Slave running on mesh partition: 2 Job started: Thu Jan 10 10:18:45 2008 +--------------------------------------------------------------------+ | Memory Allocated for Run (Actual usage may be less) | +--------------------------------------------------------------------+ Allocated storage in: Kwords Words/Node Words/Elem Kbytes Bytes/Node Partition | Real | Integer | Character| Logical | Double ----------+------------+------------+----------+----------+---------- 1 | 37987.2 | 6495.2 | 2447.4 | 40.0 | 957.2 | 473.22 | 80.91 | 30.49 | 0.50 | 11.92 | 958.52 | 163.89 | 61.75 | 1.01 | 24.15 | 148387.6 | 25371.8 | 2390.0 | 39.1 | 7478.2 | 1892.88 | 323.65 | 30.49 | 0.50 | 95.39 ----------+------------+------------+----------+----------+---------- 2 | 37941.5 | 6487.8 | 2447.4 | 40.0 | 957.2 | 473.10 | 80.90 | 30.52 | 0.50 | 11.94 | 958.43 | 163.89 | 61.82 | 1.01 | 24.18 | 148209.1 | 25342.8 | 2390.0 | 39.1 | 7478.2 | 1892.39 | 323.59 | 30.52 | 0.50 | 95.48 ----------+------------+------------+----------+----------+---------- Total | 75928.8 | 12982.9 | 4894.8 | 80.0 | 1914.4 | 474.55 | 81.14 | 30.59 | 0.50 | 11.97 | 959.90 | 164.13 | 61.88 | 1.01 | 24.20 | 296596.8 | 50714.6 | 4780.1 | 78.1 | 14956.4 | 1898.22 | 324.57 | 30.59 | 0.50 | 95.72 ----------+------------+------------+----------+----------+---------- +--------------------------------------------------------------------+ | Total Number of Nodes, Elements, and Faces | +--------------------------------------------------------------------+ Domain Name : Domain 1 Total Number of Nodes = 160000 Total Number of Elements = 79101 Total Number of Hexahedrons = 79101 Total Number of Faces = 159998 +--------------------------------------------------------------------+ | Buoyancy Reference Information | +--------------------------------------------------------------------+ Domain Group: Domain 1 Buoyancy has been activated. The absolute pressure will include hydrostatic pressure contribution, using the following reference coordinates: ( 2.50000E-03, 5.00000E-05, 5.00000E-02). +--------------------------------------------------------------------+ | Initial Conditions Supplied by Fields in the Input Files | +--------------------------------------------------------------------+ Domain Name : Domain 1 Absolute Pressure Air at 25 C | Water.Curvature Air at 25 C | Water.Interfacial Area Density Air at 25 C | Water.Surface Tension Force.Bforce Air at 25 C | Water.Unclipped Interfacial Area Density Air at 25 C.Absolute Temperature Air at 25 C.Buoyancy Force.Bforce Air at 25 C.Conservative Volume Fraction Air at 25 C.Conservative Volume Fraction.Gradient Air at 25 C.Courant Number Air at 25 C.Shear Strain Rate Air at 25 C.Smoothed Volume Fraction Air at 25 C.Smoothed Volume Fraction.Gradient Air at 25 C.Static Enthalpy Air at 25 C.Static Entropy Air at 25 C.Superficial Velocity Air at 25 C.Volume Fraction Courant Number Density Density.Gradient Pressure Pressure.Gradient Total Pressure Volume Porosity Volume of Finite Volumes Water.Absolute Temperature Water.Buoyancy Force.Bforce Water.Conservative Volume Fraction Water.Conservative Volume Fraction.Beta Water.Conservative Volume Fraction.Gradient Water.Courant Number Water.Shear Strain Rate Water.Static Enthalpy Water.Static Entropy Water.Superficial Velocity Water.Velocity Water.Velocity.Beta Water.Velocity.Gradient Water.Volume Fraction +--------------------------------------------------------------------+ | Average Scale Information | +--------------------------------------------------------------------+ Domain Name : Domain 1 Global Length = 2.9240E-03 Minimum Extent = 1.0000E-04 Maximum Extent = 5.0000E-02 Air at 25 C.Density = 1.1850E+00 Air at 25 C.Dynamic Viscosity = 1.8310E-05 Air at 25 C.Velocity = 3.6057E-02 Air at 25 C.Advection Time = 8.1095E-02 Air at 25 C.RMS Courant Number = 7.6015E-02 Air at 25 C.Maximum Courant Number = 6.8045E-01 Air at 25 C.Reynolds Number = 6.8233E+00 Air at 25 C.Mass (Conservative) = 3.3265E-10 Air at 25 C.Mass (Normalised) = 3.3265E-10 Air at 25 C.Volume = 2.8072E-10 Air at 25 C.Volume Fraction = 1.1229E-02 Water.Density = 9.9700E+02 Water.Dynamic Viscosity = 8.8990E-04 Water.Velocity = 3.6057E-02 Water.Advection Time = 8.1095E-02 Water.RMS Courant Number = 7.5096E-02 Water.Maximum Courant Number = 4.9677E-01 Water.Reynolds Number = 1.1812E+02 Water.Mass (Conservative) = 2.4645E-05 Water.Mass (Normalised) = 2.4645E-05 Water.Volume = 2.4719E-08 Water.Volume Fraction = 9.8877E-01 Water.Wave Speed = 1.6928E-01 Water.Froude Number = 2.1300E-01 +--------------------------------------------------------------------+ | The Equations Solved in This Calculation | +--------------------------------------------------------------------+ Subsystem : Momentum and Mass U-Mom-Bulk V-Mom-Bulk W-Mom-Bulk P-Vol Subsystem : Volume Fractions Mass-Water CFD Solver started: Thu Jan 10 10:19:42 2008 +--------------------------------------------------------------------+ | Convergence History | +--------------------------------------------------------------------+ |
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January 15, 2008, 17:44 |
Re: air bubble is disappear increasing time using
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#2 |
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Hi,
Some comments: You may need to look at the interface sharpening method. There are a few options, I don't know which one is best. You may want to change the default differencing scheme for the volume fraction equation. Try going to a higher order scheme. These things are unlikely to make much difference if you simulation is set up properly but are worth checking: Try double precision, tighter convergence and/or smaller timesteps. Glenn Horrocks |
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January 16, 2008, 06:24 |
Re: air bubble is disappear increasing time using
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#3 |
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Hi
Try using CFX-11, as its VOF implementation is a lot better than in in CFX-10. If the relative motion between the phases is important, you may need to use an inhomogeneous multiphase model. Also, if you are trying to capture the bubble accurately, you may need a finer mesh (look for papers by P Zwart - he is involved in writing the CFX vof model to get a better idea of required grid resolutions) -latslosh. |
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January 16, 2008, 07:37 |
Re: air bubble is disappear increasing time using
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#4 |
Guest
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Thanks,Glenn Horrocks,latslosh the suggestion is very good for me.
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June 5, 2009, 00:13 |
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#5 |
New Member
Reza
Join Date: Jun 2009
Location: Sydney
Posts: 7
Rep Power: 17 |
HI
Im trying to apply VOF on a free surface flow.can any one give me an idea of what to do ? I have not worked with VOF so i would appriciate if anyone could tell me where to find a turorial or a simple example of VOF applied on a free surface in ANSYS . thank alot |
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June 5, 2009, 02:36 |
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#6 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,870
Rep Power: 144 |
Hi,
First you should look at the flow over a bump tutorial. That's the place to start. Before I give any suggestions can you describe what you are modelling? It will determine what is important. Glenn Horrocks |
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June 5, 2009, 03:21 |
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#7 |
New Member
Reza
Join Date: Jun 2009
Location: Sydney
Posts: 7
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thanks
where can i have a look at tutorial 7 (and the bump model) ? where is it ? |
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June 5, 2009, 08:17 |
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#8 | |
Senior Member
George
Join Date: Mar 2009
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June 8, 2009, 23:01 |
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#9 |
New Member
Reza
Join Date: Jun 2009
Location: Sydney
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hi
in tuturiol 7 it has used symmetry. but Im assuming to use VOF. is there any vof examples anywhere? thanks |
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June 9, 2009, 08:59 |
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#10 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
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Hi,
???? Symmetry and free surfaces are totally different things. I seem to remember tutorial 7 uses symmetry and free surfaces. Glenn Horrocks |
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