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1、Created in COMSOL Multiphysics 5.2aTurbulent Mixing of aTrace Species This mis licensed under the COMSOL Software License Agreement 5.2a.All trademarks are the property of their respective owners. See.IntroductionThis tutorial demonstrates how mixing can be simulated in a stirred vessel by seeding a
2、trace species from a point. The flow is med using the Rotating Machinery, Fluid Flowinterface, which solves the Navier-Stokes equations on geometries with rotating parts suchas impellers. The transport of the trace species is m Species interface.ed using the Transport of DilutedMDefinitionMGE OME T
3、R YFigure 1 shows the mgeometry which is s a schematic cross section of a tank with afour-blade impeller. The tank has four baffles attached to the wall to enhance mixing. The mixer blades and the impellers are approximated to be infinitely thin. The seeding of the trace species is done at the marke
4、d point.The circle between the impeller and the tank wall is the assembly boundary where the mesh is allowed to slide when the impeller rotates.Seeding pointRotational directionAssembly boundaryFigure 1: Mgeometry.2 | TU RBULENT MIXING OF A TR A C E SP ECIES DOMAIN EQUA TION AND BO UNDA R Y CONDI T
5、I O NS The mixer fluid is water, and a rotational speed of 20 rpm is prescribed for the impeller. This rotation is achieved by prescribing the inner domain to be a rotating domain. The Rotating Machinery, Fluid Flow interface then rotates the inner domain with the prescribed rotational speed. The bo
6、undary between the inner and the outer domain is prescribed to be a continuity boundary that transfers momentum to the fluid in the outer domain.The Reynolds number based on the impeller radius and the impeller tip speed is approximately 1.9 ´ 106 which means that the flow is turbulent. The Rot
7、ating Machinery,Fluid Flow interface supports the ke turbulence mwhich is applied in this example.There are two methods to reach operating conditions. One is to accelerate the impeller up to full speed and wait for the flow to reach a quasi steady-state. This approach is simple, but can be time cons
8、uming. A computationally more efficient method is to first simulate the flow using the frozen rotor approach. Frozen rotor means that the impeller, or rotor, is frozen in position. The flow in the rotating domain is assumed to be stationary in terms of a rotating coordinate system. The effect of the
9、 rotation is then accounted for by Coriolis and centrifugal forces. This solution couples to the nonrotating parts where the flow is also assumed to be stationary, but in a nonrotating coordinate system. See the CFD Module Users Guide for more information about frozen rotor.The result of a frozen ro
10、tor simulation is an approximation to the flow at operatingconditions. The resuepends on the angular position of the impeller and cannotrepresent transient effects. It is still a very good starting condition to reach operating conditions. Quasi steady-state from a frozen rotor simulation is typicall
11、y reach within a few revolutions, while starting from zero velocity requires tens of revolutions to reach operating conditions.A trace species is a species introduced in very small quantities. It is often of a sharp color to be clearly visible even in small amounts. A trace species is not supposed t
12、o affect the flow, and hence, the flow can be solved for first and then the trace species transport solved for subsequently. Because it is the mixing at operating condition that is interesting, the trace species is introduced only once the flow is closed to fully developed, which it is after approxi
13、mately six seconds starting from the frozen rotor simulation.The seeding is med as a point source with normal distribution around the release time,t = 7.0 seconds. The absolute value of the pulse is arbitrary since the trace species does not affect the flow.3 | TU RBULENT MIXING OF A TR ACE S PECIES
14、 Results and DiscussionFigure 2 shows the frozen rotor velocity field. As expected, the highest velocity magnitude is found at the tip of the mixer blades. There are also clearly visible recirculation zones both before and behind the baffles.Figure 2: The velocity field obtained from the frozen roto
15、r simulation.Figure 3 shows the velocity field at t = 30 s. The rotor position is the same as in Figure 2, and the results in the figures are similar. There are however differences. The most notably difference is the recirculation zones before the baffles that are smaller in Figure 3 than in Figure
16、2. The size and shape of the recirculation zones for the time-dependent simulation also vary with the position of the impeller.4 | TU RBULENT MIXING OF A TR A C E SP ECIES Figure 3: A snapshot of the time-dependent velocity field at t=30 s.Figure 4 shows four snapshots of the mixing process, time ru
17、nning from top left to bottom right picture. Since the velocity is rather slow at the seeding point (see also Figure 3), the initial transport is almost isotropic from the seeding point (t = 9 s). Some trace species is however entrained in the faster velocity field in the center of the mixer and bec
18、omes thereby spread in the azimuthal direction (t = 14.7 s). It only takes a few seconds more for the trace species to be almost homogeneous distributed in the mixer. The slowest spreading is to the regions in between the impeller blades. This is a well known5 | TU RBULENT MIXING OF A TR ACE S PECIE
19、S phenomenon and is the reason to why chemical substances are commonly added as close to the impeller axis as possible.Figure 4: The mixing process. Surface plots of the trace species at t = 9, 14.7, 20.4 and 26.1 seconds.Application Library path: CFD_Module/Single-Phase_Tutorials/turbulent_mixingMi
20、ng InstructionsFrom the File, choose New.NE WIn the New window, click MWizard.MWIZAR D1 In the MWizard window, click 2D.6 | TU RBULENT MIXING OF A TR A C E SP ECIES 2 In the Select Physics tree, select Fluid Flow>Single-Phase Flow>Rotating Machinery, Fluid Flow>Rotating Machinery, Turbulent
21、 Flow, k-e (rmspf).3 Click Add.4 Click Study.5 In the Select Study tree, select Preset Studies>Frozen Rotor.6 Click Done.GEO M ETR Y 1Circle 1 (c1)1 On the Geometry toolbar, click Primitives and choose Circle.2 In the Settings window for Circle, locate the Size and Shape section.3 In the Radius t
22、ext field, type 0.5.Circle 2 (c2)1 On the Geometry toolbar, click Primitives and choose Circle.2 In the Settings window for Circle, locate the Size and Shape section.3 In the Radius text field, type 0.35.Difference 1 (dif1)1 Right-click Circle 2 (c2) and choose Build Selected.2 On the Geometry toolb
23、ar, click Booleans and Partitions and choose Difference.3 In the Settings window for Difference, locate the Difference section.4 Select the Keep input objects check box.5 Select the object c1 only.6 Find the Objects to subtract subsection. Select the Active toggle button.7 Select the object c2 only.
24、Delete Entities 1 (del1)1 In the MBuilder window, right-click Geometry 1 and choose Delete Entities.2 In the Settings window for Delete Entities, locate the Entities or Objects tsection.3 From the Geometric entity level list, choose Object.4 Select the object c1 only.ete7 | TU RBULENT MIXING OF A TR
25、 ACE S PECIES Bézier Polygon 1 (b1)1 Right-click Component 1 (comp1)>Geometry 1>Delete Entities 1 (del1) and choose Build Selected.2 On the Geometry toolbar, click Primitives and choose Bézier Polygon.3 In the Settings window for Bézier Polygon, locate the Polygon Segments secti
26、on.4 Find the Added segments subsection. Click Add Linear.5 Find the Control points subsection. In row 1, set x to -0.5.6 In row 2, set x to -0.4.Bézier Polygon 2 (b2)1 On the Geometry toolbar, click Primitives and choose Bézier Polygon.2 In the Settings window for Bézier Polygon, loc
27、ate the Polygon Segments section.3 Find the Added segments subsection. Click Add Linear.4 Find the Control points subsection. In row 1, set y to 0.5.5 In row 2, set y to 0.4.Bézier Polygon 3 (b3)1 On the Geometry toolbar, click Primitives and choose Bézier Polygon.2 In the Settings window
28、for Bézier Polygon, locate the Polygon Segments section.3 Find the Added segments subsection. Click Add Linear.4 Find the Control points subsection. In row 1, set x to 0.5.5 In row 2, set x to 0.4.Bézier Polygon 4 (b4)1 On the Geometry toolbar, click Primitives and choose Bézier Polyg
29、on.2 In the Settings window for Bézier Polygon, locate the Polygon Segments section.3 Find the Added segments subsection. Click Add Linear.4 Find the Control points subsection. In row 1, set y to -0.5.5 In row 2, set y to -0.4.Point 1 (pt1)1 On the Geometry toolbar, click Primitives and choose
30、Point.2 In the Settings window for Point, locate the Point section.3 In the x text field, type 0.3.4 In the y text field, type 0.3.8 | TU RBULENT MIXING OF A TR A C E SP ECIES Union 1 (uni1)1 On the Geometry toolbar, click Booleans and Partitions and choose Union.The final operation will later be se
31、t to Form an assembly. Union operations are therefore necessary to merge the domains and the lines.2 Select the objects dif1, pt1, b1, b3, b2, and b4 only.Bézier Polygon 5 (b5)1 On the Geometry toolbar, click Primitives and choose Bézier Polygon.2 In the Settings window for Bézier Pol
32、ygon, locate the Polygon Segments section.3 Find the Added segments subsection. Click Add Linear.4 Find the Control points subsection. In row 1, set x to -0.25.5 In row 2, set x to 0.25.Bézier Polygon 6 (b6)1 On the Geometry toolbar, click Primitives and choose Bézier Polygon.2 In the Sett
33、ings window for Bézier Polygon, locate the Polygon Segments section.3 Find the Added segments subsection. Click Add Linear.4 Find the Control points subsection. In row 1, set y to -0.25.5 In row 2, set y to 0.25.Union 2 (uni2)1 On the Geometry toolbar, click Booleans and Partitions and choose U
34、nion.2 Select the objects b6, b5, and c2 only.Form Union (fin)The boundary between the rotating and non-rotating domain must be an assembly boundary so that the parts can move relative to each other.1 In the M (fin).Builder window, under Component 1 (comp1)>Geometry 1 click Form Union2 In the Set
35、tings window for Form Union/Assembly, locate the Form Union/Assemblysection.3 From the Action list, choose Form an assembly.4 On the Geometry toolbar, click Build All.5 Click the Zoom Extents button on the Graphics toolbar.9 | TU RBULENT MIXING OF A TR ACE S PECIES AD D MA T ER IA L1 On the Holbar,
36、click Add Material to open the Add Material window.2 Go to the Add Material window.3 In the tree, select Built-In>Water, liquid.4 Click Add to Component in the window toolbar.5 On the Holbar, click Add Material to close the Add Material window.ROTA T I NG MACHINER Y, T U RBU L ENT FLO W , K- e (R
37、MSPF) Rotating Domain 11234On the Physics toolbar, click Domains and choose Rotating Domain. Select Domain 2 only.In the Settings window for Rotating Domain, locate the Rotating Domain section.In the f text field, type 201/min.Rotating Interior Wall 11 On the Physics toolbar, click Boundaries and ch
38、oose Rotating Interior Wall.2 Select Boundaries 1316 only.Interior Wall 11 On the Physics toolbar, click Boundaries and choose Interior Wall.2 Select Boundaries 14 only.Flow Continuity 1123On the Physics toolbar, in the Boundary section, click Pairs and choose Flow Continuity. In the Settings window
39、 for Flow Continuity, locate the Pair Selection section.In the Pairs list, select Identity Pair 1 (ap1).Pressure Point Constraint 11 On the Physics toolbar, click Points and choose Pressure Point Constraint. The pressure level must be specified since water is an incompressible liquid.2 Select Point
40、10 only.MESH 11 In the MBuilder window, under Component 1 (comp1) click Mesh 1.2 In the Settings window for Mesh, locate the Mesh Settings section.3 From the Element size list, choose Fine.10 | TU R B ULENT MIXING OF A TR ACE SPECIES ST UD Y 1On the Holbar, click Compute.RESUL T SVelocity (rmspf)Re-
41、create Figure 2 using the following steps.Streamline 11In the MBuilder window, under Results right-click Velocity (rmspf) and chooseStreamline.In the Settings window for Streamline, locate the Streamline Positioning section. From the Positioning list, choose Uniform density.In the Separating distanc
42、e text field, type 0.02.Locate the Coloring and Style section. From the Color list, choose White. On the Velocity (rmspf) toolbar, click Plot.Add a Time Dependent study.23456AD D S T U D Y1 On the Holbar, click Add Study to open the Add Study window.2 Go to the Add Study window.3 Find the Studies su
43、bsection. In the Select Study tree, select Preset Studies>Time Dependent.4 Click Add Study in the window toolbar.5 On the Holbar, click Add Study to close the Add Study window.ST UD Y 2Step 1: Time DependentIt is important to specify frequent enough output times for the flow field. The subsequent
44、 species simulation might otherwise be effected by interpolation errors.123In the MBuilder window, under Study 2 click Step 1: Time Dependent.In the Settings window for Time Dependent, locate the Study Settings section. In the Times text field, type 0 range(6,0.15,30).Start from the frozen rotor sol
45、ution.11 | TU RBULENT MIXING OF A TR ACE S PECIES 4 Click to expand the Values of dependent variables section. Locate the Values of Dependent Variables section. Find the Initial values of variables solved for subsection. From the Settings list, choose User controlled.5 From the Method list, choose S
46、olution.6 From the Study list, choose Study 1, Frozen Rotor.7 On the Holbar, click Compute.RESUL T SVelocity (rmspf) 1Re-create Figure 3 using the following steps.Streamline 11 In the MBuilder window, under Results right-click Velocity (rmspf) 1 and chooseStreamline.2 In the Settings window for Stre
47、amline, locate the Streamline Positioning section.3 From the Positioning list, choose Uniform density.4 In the Separating distance text field, type 0.02.5 Locate the Coloring and Style section. From the Color list, choose White.6 On the Velocity (rmspf) 1 toolbar, click Plot.DEF INI T ION SGaussian
48、Pulse 1 (gp1)1234On the Holbar, click Functions and choose Local>Gaussian Pulse.In the Settings window for Gaussian Pulse, locate the Parameters section. In the Location text field, type 7.In the Standard deviation text field, type 0.25.AD D PH YSICS 1 On the Holbar, click Add Physics to open the
49、 Add Physics window.2 Go to the Add Physics window.3 In the tree, select Chemical Species Transport>Transport of Diluted Species (tds).4 Find the Physics interfaces in study subsection. In the table, clear the Solve check box forStudy 1 and Study 2.5 Click Add to Component in the window toolbar.1
50、2 | TU R B ULENT MIXING OF A TR ACE SPECIES 6 On the Holbar, click Add Physics to close the Add Physics window.AD D S T U D Y123On the Holbar, click Add Study to open the Add Study window.Go to the Add Study window.Find the Studies subsection. In the Select Study tree, select Preset Studies>Time
51、Dependent.Find the Physics interfaces in study subsection. In the table, clear the Solve check box for the Rotating Machinery, Turbulent Flow, k-e (rmspf) interface.Click Add Study in the window toolbar.456On the Holbar, click Add Study to close the Add Study window.T R AN SPO R T OF DIL U TE D SPE
52、C IE S (T DS) On the Physics toolbar, click Rotating Machinery, Turbulent Flow, k-e (rmspf) and chooseTransport of Diluted Species (tds).Transport Properties 1In the MBuilder window, expand the Component 1 (comp1)>Transport of Diluted Species(tds) node, then click Transport Properties 1.Turbulent
53、 Mixing 11 On the Physics toolbar, click Attributes and choose Turbulent Mixing.2 In the Settings window for Turbulent Mixing, locate the Turbulent Mixing Parameterssection.3 From the nT list, choose Turbulent kinematic viscosity (rmspf/fp1).4 In the ScT text field, type 1.Transport Properties 11 In
54、 the MBuilder window, under Component 1 (comp1)>Transport of Diluted Species(tds) click Transport Properties 1.2 In the Settings window for Transport Properties, locate the M3 From the u list, choose Velocity field (rmspf).Inputs section.Continuity 11 On the Physics toolbar, in the Boundary secti
55、on, click Pairs and choose Continuity.2 In the Settings window for Continuity, locate the Pair Selection section.3 In the Pairs list, select Identity Pair 1 (ap1).13 | TU RBULENT MIXING OF A TR ACE S PECIES Thin Impermeable Barrier 11 On the Physics toolbar, click Boundaries and choose Thin Impermea
56、ble Barrier.2 Select Boundaries 14 and 1316 only.Line Mass Source 11 On the Physics toolbar, click Points and choose Line Mass Source.2 Select Point 10 only.3 In the Settings window for Line Mass Source, locate the Species Source section.4 In the q·l,c text field, type gp1(t1/s)/10.ST UD Y 3Step 1: Time DependentIn the MBuilder window, expand the Study 3 node, then click Step 1: Time Dependent.In the Se
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