Ansys12.0CFX官方教程15A.pptVIP

Chapter 15 Review and Tips,Introduction to CFX,Domain Interfaces,Domain Interfaces can be used as part of a meshing strategy as well as for connecting different domains or reference frames together Boundary conditions are created in each domain when a Domain Interface is created; generally you should not edit these directly When the mesh is different on each side of the interface a GGI (General Grid Interface) is used This will use more memory in the Solver than a continuous mesh Accuracy across a GGI interface is usually not a concern as long as the mesh length scales on each side are similar Automatic Domain Interfaces are created by CFX-Pre in some cases Always check these and dont assume that all the required Domain Interfaces have been created,Sources,Sources are used to account for physics or processes that have not been directly resolved in the simulation Momentum sources can be used to create a pressure drop (e.g. a screen, a porous material) or a pressure rise (e.g. a fan) Energy sources can account for heat added/removed from the simulation When sources are functions of the solved variable (e.g. momentum sources that are functions of velocity, energy sources that are functions of temperature) the Source Coefficient should be set The Source Coefficient must be negative otherwise the solver will diverge May need to re-write the Source so that is has a negative derivative,Transient Simulations,In a transient analysis the timestep should be small enough to capture the transient behaviour of interest Boundary conditions can be functions of time Convergence should be monitored so that each timestep is converged It is generally better to reduce the overall timestep size to improve convergence rather than increasing the number of coefficient loops Remember to create the Transient Results object before running,Turbulence,Estimate the flow Reynolds Number to determine if the flow is laminar or turbulent Check y+ values to make sure the near-wall mesh is suitable y+ 300 for a Wall Function solution y+ =2 with the SST model for a low-Re solution The SST model is a good choice for a general turbulence model Be aware of the limitations of the turbulence model chosen RANS models resolve the mean flow field, therefore a lot of transient turbulent structures are not captured These may be important when simulating noise and vibration The k-e model can give inaccurate separation predictions,Heat Transfer,High speed flows (Mach 0.2) should use the Total Energy model The double precision setting for the Solver is recommended for CHT simulations (i.e. when a solid domain is included) Always make sure energy imbalances have reached acceptable levels in CHT cases Enable Viscous Work or Viscous Dissipation if heating due to viscous effects is important If thermal radiation is modeled choose an appropriate model depending on the optical thickness Thin Wall modeling and thermal contact resistances can be set at domain interfaces,Moving Zones,Moving boundaries can be simulated in several different ways For rotating walls, a wall velocity can simply be imposed if the motion is purely tangential (e.g. a rotating hub or a solid brake disk) When the rotating walls have a normal component of velocity they must be placed inside a rotating domain (e.g. blades, vented brake disk) Stationary walls then become counter-rotating in the rotating domain and must form surfaces of revolution (i.e. no normal component of velocity) Although a Mesh Motion approach is possible, it is much more computationally expensive Mesh motion is usually used to simulate deforming boundaries or linear / cyclic motion,Moving Zones,At a change in reference frame a frame change model is used From low fidelity/cost to high fidelity/cost the choices are Frozen Rotor, Stage or Transient Rotor Stator Other approaches for moving regions are: Rigid Body Motion A 6-DOF solves calculates the solid body motion Used in conjunction with Mesh Motion Immersed Solid Used to simulate moving solids that cannot be accommodated with Mesh Motion,Why Does My Case Fail in the Solver?,First carefully read the error message The error message may recommend setting an Expert Parameter This may be an appropriate fix, or it may mask an underlying problem Example: +-+ | Checking for Isolated Fluid Regions | +-+ 2 isolated fluid regions were found in domain R1 turn off this check by setting the expert parameter “check isolated regions = f“. This error usually means domain interfaces are missing, so setting the expert parameter would not usually be appropriate,Why Does My Case Fail in the Solver?,“Insufficient Memory Allocated” type errors First check the .out file to see which process was running (Solver, Partitioner or Interpolator) Increase the Memory Alloc Factor in the Solver Manager (Define Run enable Show Advanced Controls Solver / Partitioner / Interpolator tab) “Not enough free memory is currently available on the system” A system limitation has been reached! “Memory” refers to RAM Possible solutions: Run in parallel or increase the number of partitions to distribute the memory load Reduce the memory requirements for the case Smaller mesh Fewer or smaller GGI interfaces,Why Does My Case Fail in the Solver?,“Floating point exception: Overflow” The solver has diverged Often some of the equations will show “F” instead of “OK” before the error message When this error occurs in the first few iterations perform some basic checks: Are the boundary conditions physical? Whats the Reference Pressure? What pressure is set at the boundaries? Whats the initial pressure? What direction would you expect the flow to go given the specified pressures? Reduce the timescale, particularly if the solver fails later in the run,Why Does My Case Fail in the Solver?,“Floating point exception: Overflow” Write out backup files before the failure and examine the solution fields (Pressure, Velocity, ) Look for the max / min values, they will usually be very high / low Can set the expert parameter “backup file at zero” to write out a file before the first iteration, showing the initial guess Look for the first “F” if U, V, W or P failed in the 10th iteration, but Turbulence failed in the 9th iteration, then check the turbulence field,Why Does My Case Not Converge?,Walls placed at outlets If the warning message shown to the right appears during the solution it means that flow is trying to come back in through an outlet boundary Not a problem if the message then goes away Otherwise the outlet may be located in a recirculation zone,- COEFFICIENT LOOP ITERATION = 6 CPU SECONDS = 5.754E+05 - | Equation | Rate | RMS Res | Max Res | Linear Solution | +-+-+-+-+-+ | U-Mom | 0.82 | 3.3E-06 | 3.3E-04 | 4.1E-02 OK| | V-Mom | 0.82 | 2.2E-06 | 5.6E-04 | 6.4E-02 OK| | W-Mom | 0.64 | 2.3E-06 | 9.2E-05 | 1.6E-02 OK| | P-Mass | 0.66 | 2.3E-07 | 6.9E-06 | 21.6 1.7E-01 ok| +-+-+-+-+-+ +-+ | * Notice * | | A wall has been placed at portion(s) of an OUTLET | | boundary condition (at 83.8% of the faces, 89.9% of the area) | | to prevent fluid from flowing into the domain. | | The boundary condition name is: PV33. | | The fluid name is: D2O. | | If this situation persists, consider switching | | to an Opening type boundary condition instead. | +-+ | K-TurbKE | 0.45 | 1.4E-05 | 5.9E-04 | 5.9 2.7E-07 OK| | E-Diss.K | 0.45 | 4.5E-05 | 2.8E-03 | 7.3 6.5E-06 OK| +-+-+-+-+-+,Move the outlet or use an Opening boundary Or, if the area fraction that has been “walled off” is 100%, then the local fluid pressure is likely less than the specified boundary pressure,Why Does My Case Not Converge?,Changing the timescale can help convergence Slow steady convergence may be accelerated through a larger timescale Bouncy convergence or solver failure may be fixed with a smaller timescale Sometimes simulations which are run in steady state mode will not converge even with good mesh quality and a well selected timescale If a steady state run shows oscillatory behavior of the residual plots, the flow may be transient Run the case in transient mode and observe if the residuals reduce If convergence has stalled try running in double-precision Write out the residual fields (Output Control Results Output Equation Residuals) and use Isosurfaces to look for the locations with high residuals,Setting Expert Parameters,Expert Parameter can be set in CFX-Pre, or by editing the CCL In CFX-Pre: Inset Solver Expert Parameter Most, but not all Expert Parameters are shown in CFX-Pre,Setting Expert Parameters,In CCL add the EXPERT PARAMETER: object under the FLOW: object and type in the parameter You can use the Command Editor in CFX-Pre (Tools Command Editor) to type in CCL,Mesh Refinement Studies,Errors in a co