Simcenter 3D Response Dynamics is an add-on to Pre/Post for use with Simcenter Nastran. It allows you to evaluate the dynamic responses of a structural model subjected to various loading conditions. The software calculates these responses using modal approaches.
The Response Dynamics tutorial focuses on evaluation of the dynamic displacements and stresses in a bracket used to support an electronics module in an engine compartment. It is divided into two activities:
Response Dynamics – Setting up the FEM: You prepare the simulation files and define the boundary conditions and solution options necessary for creating a solution process. You then solve the model and examine the normal modes.
Response Dynamics – Analyzing a transient event: You perform a transient analysis and review results.
For detailed information about the procedures and concepts discussed in this tutorial, see the
Response Dynamics section in the Pre/Post help.
On your desktop or the appropriate network drive, create a folder named response.
Click the link below:
Extract the files to your response folder.
The response_functions.afu file contains two excitation functions. You will have the opportunity to create these functions as part of this tutorial; however, the completed functions are included for your convenience.
Start Simcenter 3D or NX.
Open rs_bracket_1_sim1.sim.
The options you select in dialog boxes are preserved for the next time you open the same dialog box within a given session. Restore the default settings to ensure that the dialog boxes are in the expected initial state for each step of the activity.
File |
Preferences→User Interface
Options |
Reset Dialog Memory
OK |
|
Simulation Navigator
rs_bracket_1_sim1.sim
New Solution
Name |
Dynamics_Solution_1 |
Solver |
Simcenter Nastran |
Analysis Type |
Structural |
Solution Type |
SOL 103 Response Dynamics |
This is the modal analysis solution for Response Dynamics. You can also use the SOL 103 Real Eigenvalues solution, but loads are not considered.
OK |
|
Specify the result types to recover in the solution. For this activity, you will recover stress, displacement, and acceleration.
Simulation Navigator
Dynamics_Solution_1
Subcase – Dynamics
Edit
Edit (Output Requests)
Acceleration |
Enable ACCELERATION Request
Stress and Displacement are enabled by default.
OK |
Structural Output Requests dialog box |
Leave the Solution Step dialog box open for the next step.
The Solution Step dialog box is open from the previous step.
Eigenvalue Method |
Lanczos |
Edit (Lanczos Data)
Frequency Range – Lower Limit |
0 |
Number of Desired Modes |
10 |
OK |
both dialog boxes |
This combination of a lower limit, no upper limit, and a number of desired modes means the solver will calculate the lowest-frequency modes within the number of modes desired, starting from the specified lower limit.
Increasing the number of modes results in a more accurate representation of the structure, but also increases the solution time. You should include enough modes to cover your frequency range of interest.
Simulation Navigator
Constraint Container
UserDefined(1)
Add to active solution or step
The constraint is added to the Constraints container for the solution.
Add an enforced motion location to the top edge of the back face. These enforced degrees of freedom will trigger the generation of constraint modes when you solve the model. Later, you will apply an enforced motion excitation to these enforced degrees of freedom.
Simulation Navigator
Dynamics_Solution_1
Constraints
New Constraint→Enforced Motion Location
Method (Top Border bar) |
Feature Edge Nodes |
an element edge along the top edge of the bracket
All nodes along the edge are selected.
DOF3 |
Enforced |
OK |
|
Now you are ready to solve the response dynamics solution and generate the modes.
Simulation Navigator
Dynamics_Solution_1
Solve
OK |
|
Wait until the solution is complete.
No |
Review Results dialog box |
the Information window
Cancel |
Analysis Job Monitor dialog box |
(hover over the tabbed area of the Top Border bar with the mouse)
Response Dynamics (select, if necessary)
Response Dynamics |
New Response Dynamics (Response Dynamics group)
Name |
RS_Meta_Solution_1 |
OK |
|
Notice the nodes that appear in the Simulation Navigator.
RS_Meta_Solution_1 |
Save
Simulation Navigator
Normal Modes [10] (under the RS_Meta_Solution_1 node)
Response Dynamics Details View |
|
If the Response Dynamics Details View is not visible, click the bar at the bottom of the Simulation Navigator to open it.
This panel displays the dynamic characteristics (frequency, mass, damping, and stiffness) for each normal mode solved in the response dynamics solution.
The modal representation for this model consists of 10 normal modes and 15 constraint modes. Each enforced DOF in the enforced motion location you defined earlier generated a single constraint mode. Your enforced motion location has 15 nodes with one DOF enforced, so 15 constraint modes were generated.
Normal Modes [10]
Quick View
By default, displacement magnitude results for Mode 1 are displayed.
Results |
Next Mode/Iteration (Quick Edit group)
Use the Next Mode/Iteration command to view additional modes.
Return to Model (Context group)
Home |
Simulation Navigator
Normal Modes [10] (under the RS_Meta_Solution_1 node)
Edit Damping Factor
Viscous |
4.0 |
Enter |
|
OK |
|
Response Dynamics Details View |
|
Compare the values in the Frequency column to the values in the Damped Frequency column.
Because you applied the command to the Normal Modes node, the software applies the damping to all ten modes. You can define damping for individual modes by right-clicking the mode in the Response Dynamics Details View panel and choosing Edit Damping Factor.
Normal Modes [10] (under the RS_Meta_Solution_1 node)
In the Response Dynamics Details View panel, note the mass values of each mode in the Z direction (under the %Z_Mass column).
In this simple scenario, you are interested only in the dynamic response in the Z-direction. As a general rule, you should have at least 80% representation of mass in the direction you are evaluating to achieve an accurate analysis. Modes 1, 3, and 7 are the only significant modes in the Z-direction. (In general, you can consider modes that contribute more than 0.5% to be significant.) Together, they represent 95.8% of the mass in the Z-direction.
The columns in the picture have been rearranged for clarity.
The values that you see in your model may be slightly different.
To further reduce the modal model, you can remove modes 2, 4, 5, 6, 8, 9, and 10 from the analysis because they do not contribute to the modal mass in the direction of interest.
Modes with an asterisk character (*) in the # Mode column are considered “active” in your response evaluations. By default, all modes are marked as active.
Ctrl |
+ modes 2, 4, 5, 6, 8, 9, and 10 |
Deactivate
The asterisk characters next to the selected modes disappear.
Save
Transmissibility is a frequency response function that lets you evaluate the response of one or several output nodes to an enforced motion input such as displacement, velocity, or acceleration at a selected node.
Simulation Navigator
RS_Meta_Solution_1
Evaluate Transmissibility
Result |
Displacement |
Input Motion Type |
Acceleration |
Excitation Location List (ID)
Select Excitation Location |
|
Node[number]: Z |
Select an ID number in the Select Excitation Location dialog box that corresponds to a node near the center of the top edge of the back face. The node that you select is highlighted in the graphics window (see below). Because you will need to know the ID number of this node later in this activity, write it down.
The ID number in your model will be different from that shown in the illustration.
OK |
Select Excitation Location dialog box |
Input Direction |
|
Data Component |
Z |
Z is the only selectable direction because your enforced motion location was defined in the Z direction.
You cannot use the Evaluate FRF command because FRF evaluates frequency response to a unit force load, and, in this case, the load point is grounded with the enforced motion location constraint. You cannot use the same model to apply a force and displacement (or acceleration) to the same node.
Leave the Evaluate Transmissibility dialog box open for the next step.
The Evaluate Transmissibility dialog box is still open from the previous step.
Output Nodes |
|
Node (Select Node)
(the two opposite corner nodes and the CONM2 element)
Output Request |
|
Data Component |
Z |
Leave the Evaluate Transmissibility dialog box open for the next step.
The Evaluate Transmissibility dialog box is still open from the previous step.
Property |
|
Range (Method)
Frequency Start Value |
0 |
Frequency End Value |
40 |
This frequency range should cover the frequency of the 3 active normal modes.
OK |
|
Create New Window (Viewport dialog bar)
Notice the first peak in the graph; it is the zero-frequency response. But because of the frequency increment, it does not appear at 0 Hz. In the next step, you will fix this issue.
Graph Window 1
Increase the resolution of the graph by adding spectral lines.
Repeat the previous steps to evaluate transmissibility.
Select the same enforced motion location and output nodes that you used in the previous steps, and use the same values in the Evaluate Transmissibility dialog box (which should be preserved from the previous steps).
Additional Spectral Lines |
1000 |
OK |
|
Create New Window (Viewport dialog bar)
Graph Window 1
Save
This step concludes the first Response Dynamics tutorial. If you plan to continue now with the Response Dynamics – Analyzing a transient event tutorial, leave the Simulation file open. Otherwise, retain the files from this completed activity because you will need them for the next tutorial.