CATIA V5R21 FOR ENGINEERS AND DESIGNERS PDF

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Catia V5r21 For Engineers And Designers Pdf

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Strain energy is helpful in finding the area that is most affected by the vibration pattern from a natural frequency. Mode 2 Primary Bending Double click 1 Translational displacement Mode 3 Torsion magnitude to edit 8.

View the displayed frequency under tab - Frequencies. Mode 4 Secondary Bending Select and examine each mode. The displacement distribution and Frequency is what we want. Visualize the analysis results Animate all 5 dynamic modes. The Translational displacement magnitude image must be active. Select the Animate an Analysis Image 5 icon. Select Current 4 Occurrence to know what mode you are 3 animating. Select different mode numbers and select OK. Use the controls in 2 the Animate Window to animate the image.

Visualize the analysis results Mode 5 has the greatest displacement, locate the element of maximum strain energy. The Translational displacement 5 magnitude image must be active. Then double 1 clicked. Select mode number 5 to make it the current occurrence, select OK. Location and value are displayed.

Generate a report 4 After activating each mode image at least once, generate a report. If parabolic elements were used Steps: If a structure has N 1 dynamic degrees of freedom there are N natural frequencies.

Highlight document. Click Save As to specify name and path…OK. Be conservative by using a design case of lbs forward on the seat. Apply material properties to all parts. Examine and verify assembly constraints.

Create an assembly static analysis document. Apply Property Connections. Apply a moment load. Compute a Frequency Modal analysis for the assembly. Generate a report. Appendix showing precise results. Open the ws7seatPOSTassy by double-clicking.

Apply material properties to all parts Steps: Select Aluminum, select OK. Make certain material is applied properly in the tree. Apply Steel to the lower and upper clamp parts. Double click 2 seatPOSTassy to access the assembly workbench. Examine and verify assembly constraints 2 3 Assembly product.

Part Instance. Actual Part. You should be in the Assembly design workbench. Notice the small differences in icons. These are your main assembly tools. Examine the Fix. Assembly constraints should start with an anchor.

Examine and verify assembly constraints Examine constraints between the post and lower clamp. Select the Wireframe NHR visualization option. Highlight each constraint separately. A good check is to move parts around arbitrarily with the compass and then update. Also, stress analysis property connections are applied to these assembly constraints. The goal is to setup a statically determinate 1 model.

Examine and verify assembly constraints 1 Examine upper clamp constraints. Create an assembly static analysis document 1 4 Just like before. From Start menu select a Generative Structural Analysis workbench.

One difference to notice is the available Connection icons. Create an assembly static analysis document Specify unique 2 External Storage directory locations. Modify the Results Storage Location and rename as shown. Pre-process initial finite element mesh Define Linear global finite element mesh properties for all parts. Specify global mesh and sag as shown for the post, select OK. Specify global mesh and sag as shown for the clamps, select OK.

Each part can have unique element types. The Linear element is suggested for computational speed until we achieve a statically determinate model. Select the Fastened Connection icon. From the tree select the surface contact post. Note the mesh connection created between parts and a contact property. Apply a clamp restraint 1 We only want to clamp the bottom 4 inches of the post. Modification of the post. CATPart is required. CATProd uct. This changes your active document and Clamping launches you into the requirement Assembly Design Workbench.

Select the sketcher icon and the xy plane. Activate the custom 4 display mode. Continued on next page. Apply a clamp restraint 2 Sketch a shape. Select the normal view icon to see the bottom if necessary.

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Select the circle 1 icon and create a circle as shown. Apply a clamp restraint 4 1 Constrain circle. Select the constraint icon. Select the circle previously created, 2 then the post outside diameter. Result 4. Select the exit 3 sketcher icon, this takes you back to the Part Design workbench. Apply a clamp restraint 1 Create a surface that exactly represents your clamping area.. Select the Extrude icon. Select the sketch you previously created as the Profile. Key in limits as shown, select OK.

Apply a clamp restraint 1 Sewing the Extrude. Select the sewing 3 2a icon, then select the Extrude. Make sure arrows 2b are pointing in, select OK. Finally no-show the incorrect Correct Extrude. Apply a clamp restraint 1 3 2 Steps: Select the post area 4 inches that we just sewed a surface on, select OK. The clamp only applies to the bottom 4 inches. Note the Clamp object added to the features tree.

Select the Moment icon. Select the 4 faces where the seat attaches. Enter inch lbs 3 about the y-axis lb x 7 inches.

Note the Moment. Compute the analysis 3 Debugging singularities. Double click on the 2 Static Case Solution. Compute All, select OK.

Note the resources estimation, select Yes. Singularity detected, select OK. Compute the analysis 2 Visualize what causes the singularities so you can properly 1 restrain your system. Select the 3 Deformation icon. Note the upper clamp part requires a restraint. In the features tree right click Deformed Mesh object then select Inactivate. Compute the analysis 1 Define the second Fastener Connection making our model statically determinate.

From the tree select the surface contact lower clamp. Note the mesh connection created between parts and contact properties. Compute the analysis 2 Show the Deformed Mesh. Note the resources 3 estimation, select Yes. Note all images are available. Activate the Deformed Mesh image. Animate to visualize behavior. Select the Von Mises 3 Icon. Select on the Search Image Extrema icon.

Select Global and request 2 maximum extrema at most, select OK. Select Cut Plane Analysis Icon. Use the compass to locate the cutting plane as shown. Modify the cut plane options to your liking, select close. Steps 1. Next we will verify the estimated error to know this is the precise design stress. Select the display stress estimated precision Icon.

Select Estimated local error in the features tree. It is important to note that the estimated maximum global error 1 is not near the critical clamping area. Verify that the Estimated Error image 3 is active, and select the Adaptivity box Icon.

Locate and size the adaptivity box as shown. Note the Local Error In the interest of time, stay with linear elements for this class. Visualize the analysis results 3 Visualize the assembled Displacement image.

Select the Displacement Image Icon. Double click 2 Translational displacement object in the features tree to edit image parameters.

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Visualize the analysis results 5b Visualize the Von Mises stress for the post. Select the Von Mises icon this deactivates the active image and actives Von Mises. Double click Von 2 3 Mises in the features tree to edit the image.

Right click Extrema in features tree then select Local update. Right click Global Maximum. Double click to see the image extremum editor.

Visualize the analysis results 4b Visualize the Von Mises stress for the lower Clamp. Double click Von Mises in the features 1 tree to edit the image. Right click Extrema 2 in features tree then select Local update. Visualize the analysis results 4b Visualize the Von Mises stress for the upper Clamp. Visualize the analysis results Visualize the Von Mises stress localized 2a at the clamp. Verify the Von Mises Stress image is active.

Then double click to edit the image in the features tree. Select the Selections tab, then the Clamp. Also examine the Moment. Visualize the analysis results 3 2 Find the Reactions in the clamped area. Right click the Sensor. Double click Reaction-Clamp.

Select the Moment tab, verify that it equals the induced moment, select close. Visualize the analysis results Find the Bolt Loads.

Right click the 3 Sensor. In Reaction sensor select Fastened 5 Connection. Change Reference 6 Axis Type to User. Re-compute to update newly created sensors. Double click Reaction-Fastened Connection. Frequency Modal analysis for the assembly 3 4 1 2 Start by inserting a new frequency analysis with restraints.

From the Insert menu select Frequency Case. Select reference to use static case restraints. Select static restraints from features tree to specify reference select OK. Frequency Modal analysis for the assembly 3 2 Create mass equipment. Select the mass 1 icon. Select four inner faces as the supports. Key in lb as the mass, select OK. Frequency Modal analysis for the assembly 2 Specify solution 1 parameters. Double click Frequency Case Solution.

Key in 5 number of modes. Select the lanczos method, select OK 3. Select the compute icon and specify All, select OK. Frequency Modal analysis for the assembly 3a Visualize the results. Select the Displacement image icon.

Double click Translational displacement in the 2 features tree to edit image parameters. Click the Frequencies tab and select mode numbers to view each image. To view displacement at any calculated mode, animate. Repeat with other modes. Generate a report Conclusions: Maximum stress exceeds material yield. Select new material with yield values that exceed the analyzed Von Mises extrema using the parabolic element results.

Von Mises extrema Von Mises extrema Linear elements, Select the Basic 3 Analysis Report icon. Key in Title of the report. Choose both analysis cases, select OK. Generate a report 1 2 Report features Steps: If your report does not automatically launch locate the.

Selecting a topic, will launch the report specifically locating your area of interest. It may launch minimized. From File menu select Save Management. Click Save As to specify name and path, select OK. Check global and local precision animate deformation, adaptive boxes and extremas.

Change mesh to parabolic. Compute the precise analysis. Visualize final results. Open the existing ws8rectangularBeam. C 2 ATPart from the training directory. Apply steel material properties to the part as required. Launch the Generative Structural Analysis workbench. Specify the Computations and Results storage locations as shown.

Mesh globally with linear elements 2 3 4 Compute and visualize the mesh only Steps: Select the compute 1 icon and compute mesh only, select OK 2.

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Right click Finite element Model in the features tree then select Mesh Visualization. Note the image that get added to the features tree. Mesh globally with linear elements 1 Better visualize the 2 mesh by turning off the material rendering.

Click the Facet box, select OK this will turn off the Materials rendering. This icon shows your customized view 3 4 parameters. The dynamic hidden line removal image shows only the outside elements. Mesh globally with linear elements 1 Better visualize by shrinking the mesh elements. Double click the 2 Mesh object in the features tree. Slide the Shrink Coefficient bar to 0. Apply a clamp restraint 3 1 Steps: Change your display mode to Shading with Edges.

Select the face at the origin, select OK. Apply a clamp restraint 3 Examine the details of what this clamp feature is doing at the nodes. Re-compute Mesh only. Display geometry with the Dynamic Hidden Line Removal icon. Right click the Clamp.

Apply a clamp restraint 1 2 Further examine the details of what this clamp feature is doing at the nodes. Double click the Mesh object in the features tree. Symbol indicates clamped, 2. Select the or all 6 degrees of freedom restricted. Selections tab and Clamp. Display geometry 4 with the Dynamic Hidden Line Removal icon. Apply a distributed force 1 Steps: Select end face as shown. Apply a distributed force 3 Examine the details of what this Distributed Force. Display geometry with the Wireframe 4 NHR icon.

Right click Distributed Force. Apply a distributed force 2 1 Further examine the details of what this Distributed Force. Select the Selections tab and Distributed Force. Compute the initial analysis 2 1 Steps: Change your 4 display mode to Shading with Edges. Check global and local precision Visualize the 4b computation error 3 map. Select the Precision icon. Select on the information icon. Select the Estimated local error object in the features tree.

Check global and local precision Find the global element with the highest estimated error. Right click the Global Maximum. Select the adaptivity box icon.

Change mesh to parabolic 1 Redefine the global finite element mesh type. Compute the precise analysis 2 Steps: Compute the precise analysis Check how much the global estimated error has improved Steps: Select the 3 Estimated local error object in the features tree. Note the global 2 estimated error rate is very good.

Compute the precise analysis 3 Check how much the local estimated error has improved. Right click Extrema object in the features tree then select Local Update. Double click the Adaptivity Box. Visualize final results Add the displacement 1 image. Visualize final results Find the element with maximum displacement. Select the search 2 image extrema icon then select Global and key in 2 Maximum extrema at most.

Double click Translational 1 displacement vector in the features tree then select the filters tab. By positioning the cursor on a displacement symbol the component values show relative to the current Filter. Click on the Materials 4b box so we can render our image with solid colors. Display customized 3 view parameters. Visualize final results Visualize Von Mises stress field patterns. Select the Stress 1 Von Mises icon. This automatically deactivates the Translational displacement image and activates the Von Mises image.

Visualize final results Find the element with maximum Von Mises Stress. Right click Global 1a Maximum. Visualize final results 2b 3 Find exact recommend design stress. Double click Von Mises Stress object in the features tree. Note you are looking at stress values averaged across elements. Also by selecting the 1 4 Filters tab notice the stress output is calculated at the nodes. Visualize final results 1 Find exact recommend design stress. By positioning the cursor on a element the stress values show 3 relative to the current Filter in this case at the nodes.

The maximum extrema stress is uninfluenced by poisson effects yielding higher than expected stresses 3. The design stress is found at the intermediate nodes of the bottom elements. Visualize final results 3 Find horizontal shear stress. Select the Principal Stress icon. This automatically deactivates the Von Mises stress image and 4 activates the Principal 1 Stress image.

Double click Stress 2 principal tensor symbol object in the features tree. Visualize final results 2 Find horizontal shear stress. Hold the cursor on the tensor symbols will show the values.

Hold the Ctrl key down to select multiple values. Highest value should occur at the neutral axis. This model shows psi 2. Lowest value should occur on the outer edges. To be conservative, increase material strength to a minimum yield of psi for the described load case. Hand Calculations. Select Save Management from the 1 File menu.

Select Save As to specify name and path, select, OK. Perpendicular deflection in. Unit strain, elongation or contraction in. Unit shear strain in. Normal stress, tensile or compressive psi ; strength psi. Bending stress psi. Yield strength psi. Shear stress psi ; shear strength psi. Change mesh to parabolic, possibly add local meshing. Open the existing ws8bZsection. CATPart from the training directory. Apply aluminum material properties to the part as required.

Mesh globally with linear elements 1 2 Steps: Right click in the Global Size box and 3 select Measure.

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Note measure between is current, select the two edges indicated. Change to. Click Yes, you do want to copy result of this measure in this parameter. Apply a clamp restraint 1 2 Steps: Apply a distributed force 1 Load only on the web Steps: Select two edges as 2 shown. Apply a distributed force 1 It is necessary to add 2 a boundary condition that forces all bending to occur in the x-z plane.

Select the Surface Slider icon. Select the face as shown. Unsymmetrical sections will deflect laterally without this Surface Slider restraint. Select on the Animate icon. Front View Verify that you have no deflection in the 2 y-direction by animating the front view. Check global and local precision 3 Visualize the computation error map. Use the compass and green dots to locate and 2b size box around meshed areas. Select the Estimated local error 3 object in the features tree.

Double click the Adaptivity Process object in the features tree. Select the search image extrema icon then select Global and key in 2 Maximum extrema at most. Double click Von Mises Stress object in 2a the features tree.

Note you are looking at stress 4 values averaged across elements. Also by selecting the 1 Filters tab notice the stress output is calculated at the nodes. Visualize final results 1 2 Find exact recommend design stress. By positioning the cursor on a element the stress values show relative to the current Filter in this case at the nodes. From the file menu select Save 1 Management. Mesh globally with parabolic elements. Apply a pressure force.

Change mesh size and add local meshing. Open the existing ws9stepped. Apply steel material 2 properties to the part as required. Mesh globally with parabolic elements 1 2 Steps: Select the face as shown, select OK. Apply a pressure force 2 1 Load only on the web. Select the Pressure icon. Select top face as shown. Pressure is always normal to the surface and negative directs force outward, select OK. Check global and local precision Visualize the 1 Deformation and animate. Verify that you have no deflection in the 2 x-direction by animating the Right side view.

Use the compass and green dots to locate and size box around meshed 2a areas. Use the compass and green dots to locate and size box around the notch area. Select the Local tab and add local mesh size and sag as shown select OK. Compute the precise analysis Check how much the global estimated error has improved. Right click Extrema object in the features tree then select Local 1 Update. Select the search image extrema icon then select Global and key in 2 Maximum 2 1b extrema at most.

Visualize final results 1 Peak Stress Visualize peak and Remote Stress remote stress to verify the stress configuration factor Kt. By positioning the cursor on a element the stress values show.

Assume only pure torsion lbs 6. Apply a moment force.

Change global and local mesh size. Open the existing ws9bShaft. Apply steel material properties to the part as required remember modulus of rigidity for torsion. Mesh globally with linear elements 1 Steps: Apply a clamp restraint 2 1 Steps: Select the Clamp restraint icon. Select the 4 faces as shown, select OK.

Apply a moment force 1 3 Load only one end. Select four faces as shown. Enter lbfxin in the positive y-direction. Compute the initial analysis 1 Save first. Check global and local precision 1 Visualize the Deformation and animate. Verify that 2 deformation is what you expect. Check global and local precision 2 Find the global element with the highest estimated error. Focus On the worst 1 element. Use the compass and green dots to locate and size box around the 3 shoulder area.

Change global and local mesh size 1 Steps: Change global mesh as shown. Select the Local tab and add local mesh size and sag in the shoulder areas as shown select OK. Compute the precise analysis 1 Save first. Compute the precise analysis Check how much the global and local estimated error has improved.

Select on the information icon then Estimated local error in the features tree. Still not per the recommended 2 minimums, you could 1 try parabolic elements if you have time 2.

Visualize final results 1 Add the Rotational displacement images. Right click the Static Case Solution. Visualize final results 1 Visualize Von Mises stress field patterns. Visualize final results 2 Find the element with maximum Von Mises Stress. Select the search image extrema icon. Visualize final results Display Principal Stresses to verify maximum shear. Select the display principal stress icon.

Edit image to show only hoop or shear stress component C1. Fine tune your max shear image next page. Visualize final results Hand calculations indicate max shear of 39, psi at the shoulder, so… Steps: Double click color 1 pallet and Impose a max 39, this will color elements with 39ksi and higher red. Dig deeper, next page. Remote Stress Steps: By positioning the cursor on a element the Peak Stress stress values show. Visualize final results 2 Find global maximum shear stress.

Select the search Image extrema then focus on the element. This design stress occurs at the smaller cross section as would 1 be expected. Stress Concentration Factor 1.

Apply an advanced and isostatic restraint simply supported. Apply a line force density load. Refine the mesh locally. Open the existing ws10annularPlate. Mesh globally with parabolic elements 1 Steps: Then use localized adaptive meshing for precise results. Apply an advanced restraint 1 Steps: Select the Advanced Restraint icon and restrain only translation 3. Select the outer edge as shown, select OK.

The advanced 2 restraint allows you to fix any combination of available nodal degrees of freedom. Apply an isostatic restraint 1 Apply an Isostatic restraint. Select the Isostatic Restraint icon, select OK. This will restrain the remaining degrees of freedom required to make our part statically determinate.

Apply a line force density load 1 Steps: Select the Line 2 Force Density icon. Select the 0. Special part construction techniques are necessary to enable Line Force Density application. Apply a line force density load 1 Review the special part construction techniques that enable Line Force Density application.

Launch the Part Design workbench and enter Sketch. This sketch has a line broken specifically at the point where your force will be applied. When this sketch is rotated degrees it gives us the edge element on the part that we select. Compute the initial analysis 1 Steps: Compute All Save often. Select the 2 Deformation icon. Compute the precise analysis 1 Steps: Compute All. Visualize final results Check how much the global estimated error has improved.

Select the Estimated local error object in the features 1 tree. Note the global estimated error rate is very good. Visualize final results 3 Check how much the local estimated error has improved. Relocate the adaptivity box to the new Extrema.

Visualize final results 1 2 A new way to add images. Right click Static Case Solution. From the list of Image Choices select the Translational displacement vector.

Create an advanced restraint in the specific area with nothing restrained. Rename the dummy restraint as shown. Compute All 4. This is then used in the Image Editor under 4 the Selections tab. Everything unselected Sensors and this technique can be used with knowledgeware and optimization tools.

Visualize final results Visualize two images at once. Create an additional Translational displacement image the old way. Limit the images to show only text and vectors on the dummy restraint and the z- 2 direction. Focus on Global Maximum. Apply a force. Refine the mesh locally with an adaptivity box. Open the existing ws10bRectPlate. Globally mesh as shown. As plates typically are large using one mesh element through the thickness is a good way to start.

Apply an advanced and isostatic restraint 1 2 Steps: Select the Advanced Restraint icon, restrain the 4 bottom edges. Select isostatic restraint icon, select OK. Special construction techniques are necessary to enable you to apply a force to patterns that do not exist on parts. Make your. Sketch a 0. Fill this sketch with a surface. Continue on…. Apply a force 1 Make a solid thickness based on the surface.

Go to the Part Design Workbench. Put the Sketch and the Fill features in no- show then go back to the analysis 3 workbench. This method will not effect stress levels and will work on any shape.

Apply a force 1 Now we have a 0. Select the Force icon and the center selectable area. Use force magnitude values as shown. Compute the initial analysis Save first.

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Check global and local precision Check Deformation, and global precision. Create a deformed image and animate to verify your system deflects as expected. Check Global precision looks good. Find local precision. Use the Search Image Extrema icon.

Local precision is found using the adaptivity box icon. Locate and size the adaptivity box where you want refinement, as shown. Use only one convergence. Visualize final results 2 Steps: Check local precision again. Activate the deformation image to see the local mesh refinement.

Plug Material: Open a …CATProduct, and specify materials. Create assembly constraints. Apply analysis properties. Mesh globally and locally.

Apply an isostatic restraint. Open the existing ws11CylPressFit. CATProduct from the training directory. Apply aluminum material properties to the ws11outerCyl. CATPart as required.

Apply steel material properties to the ws11innerCyl. Create assembly constraints 1 2 If you have trouble creating a constraint it could be due to your 3 current options. Otherwise this Assistant will appear. Return to the Assembly Design workbench. Select the Fix Component icon. Select the outer cylinder. Create assembly constraints Using the Compass 1 Steps: The compass is available to assist you in creating assembly constraints. Move the 2 curser onto the red dot of the compass and it will change to crossing arrows.

Hold mouse button one down and drag it to the plugs outside face as shown, let go of mouse button one. Move the curser to the Z vector of the compass, hold button one down and drag to position shown. Create assembly constraints 1 Apply a contact constraint. Make sure the Assembly Design general update is set to 2 Manual.

Select the Contact Constraint icon. Select the inner and outer surfaces as shown. Create assembly constraints 2 Apply an offset constraint. Select the Offset Constraint icon. Select the outside coplanar faces as shown. Key in 0in zero for the Offset, select OK. Select the update icon. Click File and Save Management to save this new document, confirm names and locations of all other documents involved.

Apply analysis properties 1 Simulate a contact connection. Select the Contact Connection icon. Select the surface contact constraint from the features tree.

Key in negative 0. This negative clearance simulates an interference fit. Note the Contact Connection. Contact connections 4 define clearance or penetration boundaries between parts but otherwise move arbitrarily. Apply analysis properties 1 Simulate a smooth connection to prevent the center plug from moving or sliding out. Select the Smooth Connection icon. Select the offset constraint from the features tree, click OK.

Note the Smooth Connection. Smooth connections 3 fasten parts together so they behave as a single body while allowing deformation. Mesh globally and locally The compass is very handy when specifying 1 your mesh on an assembly of parts. It's easier to figure out tough problems faster using Chegg Study. Unlike static PDF Catia Vr for Designers solution manuals or printed answer keys, our experts show you how to solve each problem step-by-step.

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Material property seen in the specification tree 2 2. Juan Perez. Editing and Modifying Surfaces Chapter Double click Finite Element Model object 2 in the features tree to take us back to the Analysis workbench. Select Save Management from the File pull-down menu.

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