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In the Select Physics tree, select Fluid Flow > Nonisothermal Flow > Turbulent Flow > Turbulent Flow, Algebraic yPlus.
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Click Add.
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In the Select Study tree, select Preset Studies for Selected Multiphysics > Stationary, One-Way with Initialization NITF.
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Browse to the model’s Application Libraries folder and double-click the file air_cooled_bess_geom_sequence.mph.
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In the Model Builder window, expand the Component 1 (comp1) > Definitions > View 1 node, then click View 1.
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Clear the Show grid checkbox.
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Clear the Show axis orientation checkbox.
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Select the Direct shadows checkbox.
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Browse to the model’s Application Libraries folder and double-click the file air_cooled_bess_model_parameters.txt.
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Go to the Add Material window.
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Click the Add to Component button in the window toolbar.
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Go to the Add Material window.
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Click the Add to Component button in the window toolbar.
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Go to the Add Material window.
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Click the Add to Component button in the window toolbar.
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In the Model Builder window, under Component 1 (comp1) > Turbulent Flow, Algebraic yPlus (spf) click Initial Values 1.
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Specify the u vector as
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Browse to the model’s Application Libraries folder and double-click the file air_cooled_bess_cabinet_fan_curve.txt.
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In the Model Builder window, under Component 1 (comp1) > Turbulent Flow, Algebraic yPlus (spf), Ctrl-click to select Fan 1 and Fan 2.
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Right-click and choose Group.
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In the Model Builder window, under Component 1 (comp1) > Turbulent Flow, Algebraic yPlus (spf), Ctrl-click to select Grille 1, Grille 2, Grille 3, and Grille 4.
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Right-click and choose Group.
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Browse to the model’s Application Libraries folder and double-click the file air_cooled_bess_module_fan_curve.txt.
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In the Model Builder window, under Component 1 (comp1) > Turbulent Flow, Algebraic yPlus (spf), Ctrl-click to select Interior Fan 1, Interior Fan 2, Interior Fan 3, Interior Fan 4, and Interior Fan 5.
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Right-click and choose Group.
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In the Model Builder window, under Component 1 (comp1) > Turbulent Flow, Algebraic yPlus (spf), Ctrl-click to select Screen 1, Screen 2, Screen 3, Screen 4, and Screen 5.
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Right-click and choose Group.
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In the Model Builder window, under Component 1 (comp1) > Heat Transfer in Fluids (ht) click Initial Values 1.
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From the list, choose Horizontal plate, upside.
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Click to expand the Corner Settings section. From the Handling of sharp edges list, choose Trimming.
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Click
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Clear the Generate default plots checkbox.
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Click OK.
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Browse to the model’s Application Libraries folder and double-click the file air_cooled_bess_cabinet_fan_curve.txt.
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Locate the Column Headers section. In the table, enter the following settings:
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Browse to the model’s Application Libraries folder and double-click the file air_cooled_bess_module_fan_curve.txt.
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Locate the Column Headers section. In the table, enter the following settings:
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Clear the Headers checkbox.
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Select the Show legends checkbox.
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Go to the Result Templates window.
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In the tree, select Study 1/Solution 1 (sol1) > Turbulent Flow, Algebraic yPlus > Wall Resolution (spf).
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Click the Add Result Template button in the window toolbar.
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Select the Show units checkbox.
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Locate the Coloring and Style section. Find the Line style subsection. From the Type list, choose Ribbon.
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Locate the Position section. In the z text field, type Gap_bottom_modules+2*H_module+1.5*Gap_z_modules.
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Locate the Position section. In the z text field, type Gap_bottom_modules+3*H_module+2.5*Gap_z_modules.
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Locate the Position section. In the z text field, type Gap_bottom_modules+4*H_module+3.5*Gap_z_modules.
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In the Settings window for 3D Plot Group, type Module Temperature and Fluid Flow in the Label text field.
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Select the Show units checkbox.
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Locate the Coloring and Style section. Find the Line style subsection. From the Type list, choose Ribbon.
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In the Model Builder window, under Results > Module Temperature and Fluid Flow right-click Volume 1 and choose Duplicate.
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In the Model Builder window, under Results > Module Temperature and Fluid Flow right-click Streamline 1 and choose Duplicate.
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In the Settings window for 2D Plot Group, type Cross Section of the Bottom Module in the Label text field.
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Select the Show units checkbox.
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Browse to the model’s Application Libraries folder and double-click the file air_cooled_bess_geom_parameters.txt.
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On the object blk1, select Boundary 2 only.
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Locate the Selections of Resulting Entities section. Find the Selections from plane geometry subsection. Select the Show in physics checkbox.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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In the Model Builder window, collapse the Component 1 (comp1) > Geometry 1 > Work Plane 1 (wp1) node.
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On the object blk1, select Boundary 3 only.
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Click to expand the Local Coordinate System section. From the Origin list, choose Vertex projection.
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On the object blk1, select Point 1 only.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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Locate the Position section. In the xw text field, type (L_module-(L_cell+Gap_x_cells)*(Nx_cells-2)-W_hole)/2.
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In the Model Builder window, collapse the Component 1 (comp1) > Geometry 1 > Module Side Openings (wp2) node.
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Clear the Keep input objects checkbox.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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Locate the Position section. In the x text field, type (L_module-(L_cell+Gap_x_cells)*Nx_cells+Gap_x_cells)/2.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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Locate the Position section. In the x text field, type (L_module-(L_cell+Gap_x_cells)*Nx_cells+Gap_x_cells)/2+L_cell.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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Click OK.
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In the Add dialog, in the Selections to subtract list, choose Module Grill (Work Plane 1), Module Fan (Work Plane 1), and Module Side Openings.
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Click OK.
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In the Settings window for Difference Selection, type Module Aluminum Walls in the Label text field.
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Click OK.
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Click OK.
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Click OK.
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In the Model Builder window, under Component 1 (comp1) > Geometry 1, Ctrl-click to select Block 1 (blk1), Work Plane 1 (wp1), Move 1 (mov1), Module Side Openings (wp2), Copy 1 (copy1), Module Housing (uni1), Cells (blk2), Gaps (blk3), Array 1 (arr1), Array 2 (arr2), Module Walls (difsel1), Module Aluminum Walls (difsel2), and Battery Module (unisel1).
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Right-click and choose Group.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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On the object blk4, select Boundary 2 only.
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Locate the Selections of Resulting Entities section. Find the Selections from plane geometry subsection. Select the Show in physics checkbox.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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8
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Click
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6
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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7
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8
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Click
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Click
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In the Model Builder window, collapse the Component 1 (comp1) > Geometry 1 > Work Plane 3 (wp3) node.
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Click
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In the Add dialog, in the Selections to add list, choose Cabinet Housing, Cabinet Grills (Work Plane 3), and Cabinet Fans (Work Plane 3).
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6
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Click OK.
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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5
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Click
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Click OK.
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7
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Locate the Selections of Resulting Entities section. Select the Resulting objects selection checkbox.
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8
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10
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Click
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5
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Click
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Click OK.
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7
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9
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In the Add dialog, in the Selections to subtract list, choose Cabinet Grills (Work Plane 3) and Cabinet Fans (Work Plane 3).
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10
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Click OK.
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Click
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Click OK.
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10
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Click
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Click OK.
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10
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Click OK.
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Click OK.
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6
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Click OK.
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6
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Click OK.
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Click OK.
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Click OK.
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Click
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Click OK.
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Click
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Click OK.
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8
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9
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Click
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Click OK.
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7
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Click
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In the Add dialog, in the Selections list, choose Module Grill (Work Plane 1) and Module Side Openings.
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7
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Click OK.
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8
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9
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In the Model Builder window, under Component 1 (comp1) > Geometry 1 right-click Bottom Module (boxsel4) and choose Duplicate.
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2
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3
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Locate the Box Limits section. In the z minimum text field, type 0.99*(Nz_modules-1)*(H_module+Gap_z_modules)+Gap_bottom_modules.
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4
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In the z maximum text field, type 0.99*(Nz_modules-1)*(H_module+Gap_z_modules)+Gap_bottom_modules+H_module.
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1
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In the Model Builder window, under Component 1 (comp1) > Geometry 1 right-click Bottom Cells (boxsel5) and choose Duplicate.
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2
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3
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Locate the Box Limits section. In the z minimum text field, type 0.99*(Nz_modules-1)*(H_module+Gap_z_modules)+Gap_bottom_modules.
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4
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In the z maximum text field, type 0.99*(Nz_modules-1)*(H_module+Gap_z_modules)+Gap_bottom_modules+H_module.
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1
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In the Model Builder window, under Component 1 (comp1) > Geometry 1 right-click Bottom Module Openings (boxsel6) and choose Duplicate.
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2
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3
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Locate the Box Limits section. In the z maximum text field, type 0.99*(Nz_modules-1)*(H_module+Gap_z_modules)+Gap_bottom_modules+H_module.
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4
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Click
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7
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Click OK.
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8
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10
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1
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2
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In the Settings window for Difference Selection, type Cabinet Frontside Walls in the Label text field.
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Click OK.
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10
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Click OK.
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