why my momentum and mass not convergence
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dear all, my case is simulate the the fan in an tools, i just want to know the massflow, but i can not get the right result ,since the RMS not convergence even more than 1000 iterations. the parameters is copied below, LIBRARY: 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: 。。。。。。。。。。。。。。 END END END FLOW: Flow Analysis 1 SOLUTION UNITS: Angle Units = [rad] Length Units = [m] Mass Units = [g] Solid Angle Units = [sr] Temperature Units = [K] Time Units = [s] END ANALYSIS TYPE: Option = Steady State EXTERNAL SOLVER COUPLING: Option = None END END DOMAIN: housing Coord Frame = Coord 0 Domain Type = Fluid Location = DOMAIN_OF_STATOR BOUNDARY: Default Fluid Fluid Interface Side 1 Boundary Type = INTERFACE Location = Primitive 2D AS,Primitive 2D AT,Primitive 2D AU,Primitive \ 2D AV,Primitive 2D R,Primitive 2D S,Primitive 2D T,Primitive 2D U BOUNDARY CONDITIONS: MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END BOUNDARY: baffle Boundary Type = WALL Location = BAFFLE BOUNDARY CONDITIONS: MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: brakets Boundary Type = WALL Location = BRACKETS BOUNDARY CONDITIONS: MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: housing Default Boundary Type = WALL Location = HEAT_SINK,MOSFET1,MOSFET2,PCB BOUNDARY CONDITIONS: MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END 。。。。。。。。。。。。。。 BOUNDARY: inlet Boundary Type = OPENING Location = INLET,INLET2 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 TURBULENCE: Option = Medium Intensity and Eddy Viscosity Ratio END END END 。。。。。。。。。。。。。 BOUNDARY: outlet Boundary Type = OUTLET Location = OPENING BOUNDARY CONDITIONS: FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Option = Average Static Pressure Pressure Profile Blend = 0.05 Relative Pressure = 0 [Pa] END 。。。。。。。。。。。。。 DOMAIN: rotor domain Coord Frame = Coord 0 Domain Type = Fluid Location = DOMAIN_OF_ROTOR BOUNDARY: Default Fluid Fluid Interface Side 2 Boundary Type = INTERFACE Location = Primitive 2D AO,Primitive 2D AP,Primitive 2D AQ,Primitive \ 2D AR,Primitive 2D AW,Primitive 2D AX,Primitive 2D AY,Primitive 2D AZ BOUNDARY CONDITIONS: MASS AND MOMENTUM: Option = Conservative Interface Flux END TURBULENCE: Option = Conservative Interface Flux END END END END CONVERGENCE CONTROL: Maximum Number of Iterations = 500 Minimum Number of Iterations = 1 Physical Timescale = 0.01 [s] Timescale Control = Physical Timescale END CONVERGENCE CRITERIA: Residual Target = 0.00001 Residual Type = RMS END DYNAMIC MODEL CONTROL: Global Dynamic Model Control = On END END END 。。。。。。。。。。。。 Memory Allocation Factor = 1.0 END END 。。。。。。。。。。。。 |
the fluid domain
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the fluid domain
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Is that a Generator you are trying to model?..
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