I am currently doing the analysis of the frequency response of the nonlinear vibration with flexible PCB by using the module transient structural. But the problem is that I always get the linear results, I turn on the large deflection and nonlinear effects, I use the nonlinear mechanical with the element order of quadratic and the sizing function of adaptive to do the mesh. could someone give me some help, I had tried for a very long time, while I still did not get any satisfactory results.
How to do the frequency response of the nonlinear vibration of a flexible PCB?
- 1.8K Views
- Last Post 20 September 2018
- Topic Is Solved
Please reply with a sketch of the part, the supports for the part and the transient load on the part.
Please describe what in this model makes it nonlinear.
It's a good idea to do a Harmonic Response analysis before you use Transient Structural. Have you done that?
If you can share the model, attach a Workbench Project Archive after you post your reply, and say what version of ANSYS you are using.
The nonlinearity of the flexible PCB is large deformation(geometrically) and material nonlinearity.
The external load function is:
sigSweep = .5*cos((startFreq*sweepTime+((stopFreq-startFreq)/stopTime/2)*sweepTime.^2));
The two rectangular beams on the sides are the fixed support, and I would like to give it a base excitation on the two beams on the sides, but I am not sure how to do it correctly. so I change the BCs into the two beams on the side fixed rotation and the displacement with only Z is non-zero. the external excitation will also be applied at the two beams and it is sine sweeping function.
I do did the harmonic response, which give me some nonlinear effects on some special situation if I give different damping and number of steps. I have no idea why it will have nonlinear effect?
Here is a relevant discussion on a student who wants to build a simulation of an object on a shaker table. You might find that interesting.
First observation on opening your file, looking at the Transient Structural, you have a mesh that is much finer than necessary to study frequencies up to 200 Hz. I changed the max face size from 0.1 to 1 mm and deleted the Face Meshing - Triangles. The finer mesh makes you wait longer for a solution, without giving your any benefit in higher accuracy. Not sure why you thought Triangles were better than Quad elements. They are not.
Second observation, delete Fixed Rotation 2 on the face. That is not needed. You only need the ends.
After making the above two changes, I added a Modal analysis to the Transient Structural, and found the first undamped natural frequency is 264 Hz. From your Harmonic Response analysis, you are interested in 80 - 200 Hz range of frequencies. If this is the range of interest, then there won't me much response in this range. The third change I made was to change the thickness of the sheet from 0.5 to 0.125 mm. Now there are at least a few modes that are between 80 and 200 Hz.
From your Transient, you were wanting to perform a sweep over the 80 - 200 Hz range in 10 seconds.
You can apply the displacement directly to the edges as you have done. However, you must provide a minimum of 10 and preferably 20 data points per period in the input data to faithfully reconstruct a smooth signal. Since you are going to 200 Hz, that means you should have between 2000 and 4000 data points in the last second. You have only 500 data points for the entire 10 seconds, entirely inadequate! At a constant 4,000 Hz sampling rate, you will end up with 40,000 data points for the 10 second sweep.
The very first cycle has an effect on the high frequency transients you can introduce unwittingly to the simulation. If you use a sine function on the displacement, at time zero, you create a step change in velocity, which introduces high frequency noise into your results. This will die out due to damping, but your first fraction of a second will not have the valid data you want. If instead you use a cosine function, the displacement and velocity can be zero at time zero, and the velocity can ramp up (in a sine function), and you will avoid generating high frequency noise into your results. Your displacement function has a displacement of 5 mm at time zero. That is not where you want to start. You want displacement of zero at time zero. See this post for an example.
On a shaker table, the sine sweep is usually based on acceleration, not displacement. The reason is that the acceleration required to have a 5 mm amplitude is much higher at 200 Hz than it is at 80 Hz. Where did the 5 mm amplitude come from? That is huge at these frequencies. At 80 Hz, the board will experience 129 G of acceleration, while at 200 Hz, a 10 mm peak-to-peak displacement requires 805 G of acceleration. I'm sure that is not what you want. Here is the calculator I used.
Let's say you want 5 G of acceleration applied over the range 80 - 200 Hz over a 10 second time. I have a signal generating script that runs in matlab that is part of a package called vibrationdata by Tom Irvine.
This generates an acceleration signal, which can be double integrated to displacement using another script. Notice how the displacement is reduced as the frequency increases over time.
Attached is a zip file and inside is a text file with the displacement data from the graph above.
It's not based on the sigSweep external load function. I don't know what units that function is using.
One more idea: you can use fixed supports at each end and have an acceleration load, which is the original data that was generated by matlab before I double integrated it to displacement. I can provide an acceleration file or a displacement file with different settings if you want.
If you have no nonlinear materials, then you can put a Modal analysis first and feed that solution into the setup cell on the Transient Structural, then run the linear MSUP transient solution, which may run a bit faster. The Transient Structural will take an Acceleration load, but not a non-zero Displacement if it is using the MSUP solution.
Thanks for your helpful and patient reply.
Since I am also considering not including the nonlinear materials. Because only the geometric nonlinearity will also cause the system nonlinear. besides, you said that I need to use the sine function instead of the cosine function which will avoid the high-frequency noise that cause the data I do not want?
As for the boundary conditions, does it means that only the displacement is enough?
by the way, I turn on the large deflection and the nonlinear effects within the workbench, does it means that I make the model geometrically nonlinear?
That will be very great if you could provide me with the acceleration or displacement file with different settings.
As for a question concerning the damping, if I do not know the damping of the flexible PCB with the IC chips mounted on it, How could I deal with the damping? any suggestion?
one more question is that I also try with the 2D model with the thickness assigned for both the PC board and the IC chip(But I could not give two different surfaces on the 2D model, which means that I will miss one IC chip if I use the 2D model, How could I add another IC chip?), will it make the solving process faster, if it is, will the solution become less accurate?
sorry about that I have so many questions to ask, if 500 data points is inadequate, instead, I need to apply entirely 40000 data points, I do not think that my laptop could handle that large memory-required solution, could I try it with 10000 data points? will it cause a lot of errors?
Here is a good article. It is written with examples in another product, but the lesson is the same.
My guess is that you don't have any geometric nonlinearity for normal levels of vibration. If you have extremely high levels of acceleration, then you could get to a point where a nonlinear analysis would give a different result, but is that your intent or are you more interested in fatigue life estimates?
SINE vs COSINE
If you have fixed edges and use an acceleration load, then it is better to have a sine function so the acceleration ramps up from zero at time zero If you have edges with a tabular displacement input, then it is better to have an offset cosine function so that displacement and velocity at time zero are zero and ramp up from there.
TIME HISTORY SAMPLES
Having 40,000 time history data points is not taxing on your lowly laptop. Solving the Transient Structural without the Modal Solution and the linear assumption makes a lot more work for your laptop.
SHEET BODY MODEL INCLUDING ICs
You can slice your PCB sheet body to make an interior rectangle to represent the IC chip. You can assign a thickness, and even a different material to the interior rectangle. You can adjust the density of the IC material so that the mass of the interior rectangle matches the true mass of the two IC chips. Do you know how to Slice in DesignModeler, then make a multibody part to reconnect the two bodies into one part?
How does the IC connect to the PCB? Is it a Ball Grid Array? If so, in a very detailed model, you can model all the balls and compute the stress in the corner balls that will have the highest stress due to the bending of the PCB from the corners out.
I have read one of the most cited books, "Vibration Analysis for Electronic Equipment" by Dave S. Steinberg. He has a lot to say about PCB vibration and how to estimate the fatigue failure of IC chips mounted to the PCB under various vibration conditions. You should read it.
Having read that book, I wonder if a fixed support that includes clamped edges is realistic for your model. What is clamping the edge which such force that it prevents rotation? If the edge of the PCB card slides into a spring loaded channel, under vibration, there is little to no rotation constraint. It would be more realistic to model it as fixed displacement, but leave the edge rotation free.
Thanks very much for your help
Some other questions:
1. I have done the 2D model of the PCB with only one but not 2 IC chips mounted on it. I have no idea about how could you slice them in DesignModeler? could you please give me some help or suggestion? I will also attach the model that I have done with the SpaceClaim, After you take a look at it, you will know where my question is.
2. Like you stated, if the condition is fixed edges and the acceleration load, then you will need the sine function since at the time zero the acceleration is zero as well. while as for the condition with the fixed edges and the displacement, you would like to use the cosine function, but consin0=1, how could the input displacement be zero at time zero? did I misunderstand your points?
3. I also asked one of the professors working with vibration, he told me that the nonlinear geometry is vert important for my simulation, even I do not give any nonlinear materials, the nonlinear vibration effect will also occur. besides I have also read some papers which said that if the external load is large enough(large amplitude) then the nonlinear vibration effect will happen.while my research is only focused on the nonlinear vibratory effect(just the demonstration of the nonlinear vibration effect) still no any relation to the failure or fatigue.
4. The 3D model that simulated in the harmonic response is the real model that I would like to use, the reason why I use only the PC board is because I would like to make the problem simple and take less time to solve, then I will use both the PC board and IC chips to do the next simulation. but is it possible that I could get the nonlinear vibration effect with only the PC board?
5. Since from the modal analysis, the first mode of the PCB with the IC chips is bending, as for the meshing, I applied the nonlinear mechanical for physics preference, quad elements, curvature for sizing function, quadratic for element order and the quality-error limits-aggressive mechanical. is it good enough for the nonlinear analysis of the PCB with the IC chips?
6. The IC chips will be simplified as the rigidly connected with the PC board, there will be no any contact nonlinearity within my simulation.
1. You have done in SpaceClaim what I described as a Slice operation in DesignModeler, that is to create two surfaces. The last step is to set the Share Topology to Share. That means the mesher will have shared nodes at the common edge to hold the parts together.
2. For a displacement condition, it is an offset cosine. So the displacement would be
which is zero at time equals zero. The displacement varies between 0 and -2A.
3. As the amplitude is increased, the deviation between a linear and a geometric nonlinear solution will diverge. It doesn't hurt to turn on nonlinear effects even when the amplitude is low, it just may add extra time to the solution. Where requiring nonlinear hurts when you don't need it is when it eliminates a fast solution method such as Modal Superposition.
4. You can certainly get a nonlinear geometric effect with a surface model. It only depends on how large the amplitude of vibration is for a difference to show up. The difference may shows up because of the membrane tension that stiffens the board as it deforms due to the fixed supports on opposite edges of the board. You can use a Static Structural analysis to plot the peak deformation as a function of pressure for a linear and a nonlinear (Large Deflection) analysis. That will illustrate the size of the deformation where a significant deviation occurs.
5. The mesh can be quite low density when there are only a few modes in the frequency range of interest. As long as there are at least 10 elements along a deformed wave in the part, that is plenty.
6. Okay, good.
I see in the sketch that the clamping bars, if they are fixed by bolts or screws that are torqued down tight, that may indeed constrain rotation of the edges.
Here comes some other questions
1. sorry that I did not use the DesignModeler, since I am doing it for most of the time in SpaceClaim, It seems that I do no have the option share within the share topology, besides is it the reason the at I have the ANSYS version of 18.1 but you have the higher version of 19.1?
2. if you use the A*cos(w*t)-A, the input will not change the direction from -Z to Z, which means it will only have the negative direction all the time and the magnitude of the input will also be doubled, why do not we use the sine function for the displacement input?
3. I am trying to do the static structural, as what stated before, there will be 40000 data points in total that I could cover the high frequency effect,especially the 200HZ, on the nonlinear vibration. but given that it will be taxing for my laptop, could I use only 2000 data points? but if I do it like this way, will my result get totally distorted? do you have some suggestion?
4. like what you have mentioned before: "If you have no nonlinear materials, then you can put a Modal analysis first and feed that solution into the setup cell on the Transient Structural, then run the linear MSUP transient solution, which may run a bit faster. The Transient Structural will take an Acceleration load, but not a non-zero Displacement if it is using the MSUP solution." as far as I know, you could link the engineering data, geometry, model and solution but not the setup cell, could you please show me how could I feed the solution from the modal analysis into the setup cell on the Transient Structural? After that, will the ANSYS automatically run the MSUP transient solution or maybe I have to change some settings?
5. Every time, when I use the function setting for one of the components for the displacement, the other two will be automatically locked as free, do you know why will I have such a problem?
1. In the image, do you have two bodies? If you have one body with two faces, then you don't need to Share Topology.
2. The equation I showed has an amplitude of A and a peak-to-peak range of 2A. That is the same when you have A*sin(t). If this is a displacement input to a shaker table, what do you care if it goes down to -2A and back up to zero, or if it goes up to A and down to -A. It's the same range and the velocity is both going up and down. I don't think the PCB cares what height it is at.
3. If you do a Static Structural, you don't use 40000 data points. You apply a constant acceleration of say 100 G in the Z direction. In the Analysis Settings, Auto Time Stepping is turned On. You set the Initial, Minimum and Maximum Substeps to 100 and Solve. Request the Deformation. You can now see with 100 points on the plot. Solve it with Large Deflection On and Off and see how the shape of the plot changes. That is the nonlinear geometric effect you are looking for.
Forget about the 40000 data points. They will not tax your laptop. You could cut it to 20000 if you really want do make some change, but it will not matter either way.
4. Drag out a Modal analysis and drop it on the Project page, then drag out a Transient Structural and drop it on the Solution cell of the Modal analysis. That will create links which will define this Transient Structural as a MSUP solution and will not allow large Deflection to be used as it will be a linear analysis. Note that the Fixed Support is put into Modal and cannot be added under the Transient Structural branch.
5. When you use a function setting in a BC, then the other components are free. That is normal. You can use another BC to set the free components to be zero.
Thanks for your fast and helpful reply.
1. I do have more than 1 body, in fact I will have 3 bodies in total, one is the PC board, another two will be the IC chips that are mounted on the PC board, that is why I am asking that if I give the 2 surfaces with assigned thickness, when I try to give the material properties, I could assign it to the PC board and only one IC chip not the both, that is the problem that I could not solve, But considering that the two IC chips have almost the same material properties, I think it would not influence that much.
2. I am currently meet some problems on convergence issue, when I was doing the transient structural with my flexible PCB, if I turn on the large deflection, it will have some errors, I do use small time steps, but still have no idea why it will happen. while if I turn the large deflection off, there will be no errors and I am good to get the result, do you have and suggestion? I also attached the solver output file and the workbench file.
3. Sorry about my question about using sine or cosine function, hope it does not bother you. but very grateful for your amazing reply.
4. I have also done some research on nonlinear materials for the PCB, but I feel confused which nonlinear materials should I use in ANSYS, should I use the plasticity-multilinear isotropic Hardening? I think that will be the one that match the best with the model. besides it is not that easy to get some nonlinear materials for the PC board online, is it possible you could give me some help on it?
1. I had the sense that the two ICs were mounted on opposite sides of the PCB and occupied about the same area. In this case, the rectangle in the center of the PCB surface represents both ICs and has a density sufficient so that the mass of that center rectangle has the mass of that part of the PCB plus both ICs. There won't be three bodies but just two bodies.
2. You can see that the solver was heading for convergence on that last step, it it had just not quit after 26 iterations. That is where you introduce a Command item into the Transient Structural branch (not the Solution branch). Click the Insert Commands button,
Then type the command: NEQIT,60
This tells the solver to keep iterating for 60 attempts instead of the default 26.
3. No problem.
4. I don't think the PCB needs any plasticity or any nonlinear property. A linear isotropic elastic material is sufficient for this model.
In your Static Structural model, add an Acceleration of 250 m/s/s in the Z direction. Change the BC on the two edges to Fixed Supports. Solve with 25 minimum substeps with Large Deflection On and Off and you will be able to create this plot. This is the geometric nonlinearity you wanted to see.
Thanks for your helpful and patient reply
some other question still need your advice,
1. if I turn on the large deflection there will have nonlinear solution, if I turn it off, does it means that it is linear case?
besides, what is the meaning of turning on the nonlinear effect and thermal strain effect?
2. as you mentioned that even though I do not apply the nonlinear materials but with only linear isotropic material properties, I could still get the nonlinear vibration effect with only geometrical nonlinearity. is the reason that the geometrical had already included the nonlinear stress-strain relationship like the COMSOL example you sent it to me a few days ago which told me that the geometrical nonlinearity will also cause the stress-stiffening?
3. you are right, the IC chips are mounted on the opposite side of the PC board, therefore, my 2D model with assigned thickness could handle PC board with only one chip not both, that is why I could not make it perfect. besides when I was doing the mesh within the ANSYS, it shows me two IC chips, does it means that I will have 2 IC chips with the same material properties?
As I marked in the green color, There are only two surfaces that could be given the thickness, therefore it should have the PC board and only one chip, but from the view of mesh, it is 3 bodies(PC board and 2 IC chips). Do you know why?
Sorry that I have so many questions to ask
1. every time when I turn on the large deflection, there will come the warning as I posted following, will it have a big influence on my final results?
2. Thanks for telling me that I could also change the default iteration from 26 to 60. but why I did not find out that It is the issue of inadequate iterations from the solver.output file? but if I decrease the minimum time step, I find it out that there will be no convergence issue, does them means the same thing?
1. There are three types of structural nonlinearity: material, contact and geometric (large deflection). You can turn off geometric nonlinearity, but still have material or contact nonlinearity in the model. But if you have only linear (or no) contacts and only linear materials, then when you set Large Deflection Off, then you have a completely linear model.
I don't know what you mean by "besides, what is the meaning of turning on the nonlinear effect and thermal strain effect?"
2. Even with linear materials, there is a false stress as explained in the article above, due to large rotations in the solution that are not being properly computed. When Large Deflection is Off, the small angle assumption is used to make the computation faster. When you turn on Large Deflection, large rotations are handled properly, which takes more time to compute but then a large rotation of a sheet will not generate a false stress. In a model like yours or the skin on a drum head, even though the rotations may remain small, the deformation in the Z direction when solved with Large Deformation turned on adds tension to the drum, which reduces how far the drum head deflects under a given load. If you turn off Large Deformation, then no tension is added and the drum head deflects much more than happens in reality. That is the effect I made the plot for in my previous post.
3. You can have two ICs in the 2D model. That rectangle in the middle is assigned a different thickness and a different material than the PCB picture frame body. That rectangle in the middle represents two ICs and the PCB between them. The mass of that rectangle must equal the sum of the two ICs and the piece of PCB between them.
Thanks for your helpful and patient reply.
1. As for the nonlinear effects within the material setting, I am wondering that does it means something related to the nonlinear material properties? If I turn it off, will the model become linear materials?
2. Sorry that the 2D model issues make you feel a bit annoyed, from my understanding is that I thought there should be 3 surfaces in total that I could assign the thickness and the material properties for the PC board and IC chips. could you please give me an example with visualization or some online videos that could help me to better understand it?
1. A basic structural dynamics linear material needs density, and isotropic elasticity, which is Young's Modulus and Poisson's Ratio. You can add a nonlinear property like Plasticity, or if it is already there, you can delete the nonlinear property. There is no turning it off, just either add or delete the nonlinear property.
2. Sorry that I repeated the same explanation I used previously; that wasn't helpful.
Do you know the game of checkers? There is a checkerboard and pieces occupy squares. Some squares are empty, some have one piece on it, and some squares have a stack of two pieces on one square.
Now let's build a 2D model of that checkerboard. Take a large surface and slice it into an 8x8 grid of squares. Each square is going to be assigned one of three different materials. Let's call the materials: Empty, One and Two. Each square is also going to be assigned a thickness.
Let's say the board is 2 mm thick, and the pieces are 4 mm thick. Assign a thickness of 2 mm to the empty squares, a thickness of 6 mm to the squares that had one piece on them, and assign a thickness of 10 mm to the squares that had two pieces on them.
Let's say that one empty square of checkerboard weighs 3 grams, and each piece weighs 5 grams. When you create the material called Empty, you have to adjust the density of the material until that square surface that has been set to a thickness of 2 mm shows a weight of 3 grams. Similarly, the material called One is assigned to a square surface that has been set to a thickness of 6 mm and you have to adjust the density until that surface weighs 8 grams. Finally, the material called Two is assigned to a square surface that has been set to a thickness of 10 mm and you have to adjust the density until that surface weighs 13 grams.
At the end of building this 2D model, there will be a grid of surfaces, where each surface represents either an empty square, a square with one piece on it or a square with two pieces stacked on it. The total mass of the 2D model will exactly equal the mass of the real 3D checkerboard with the pieces on it, and the distribution of mass over the 2D surface area will closely represent the true distribution of mass over that area.
This same method can be used to make a 2D model to represent the mass and stiffness of a PCB where there may be two ICs on opposite sides of the board at one location. A more complicated board that had a single IC at another location would require a third material definition. The cutout in the board is in the shape of the IC but it is the material and thickness assignment that defines whether there are zero, one or two ICs on that cutout.
Thanks for your help reply.
1. The rectangle in the middle in fact have the total thickness of the PCB and the 2 IC chips, am I right? I also mark it in red color in the following figure, besides, I could not give different stiffness behavior for the PC board(the bigger rectangle) and the IC chip(the middle rectangle in the figure). I also attach the workbench file, Could you please help me with this problem?
I see you have two surface bodies.
- Body Thickness Material Mass
Outer 0.15 mm substrate 0.454 g
Center 2.68 mm IC chip 1.239 g
The bending stiffness of a beam depends on the factor EI, where E is Young's Modulus and I is area moment of inertia.
While both materials have the same value of E, 5000 MPa, they have very different thickness values. For a rectangular cross section of thickness t and breadth b, the formula for I is bt^3/12. So you can see that the IC is going to be much stiffer than the PCB substrate.
The thickness of 0.15 mm seems very thin for a board that has a span of 45 mm. Is it correct?
In the Static Structural model, do Fixed Supports like you did in the Modal, instead of the Displacment and Fixed Rotation you had. Then add an Acceleration load in the Z direction of 200 m/s/s. With Large Deflection turned On, you will get this plot of Deformation
In the Modal analysis, you set the stiffness behavior of the IC to rigid, but there is no need because it is already much stiffer than the PCB, and the Modal solution won't solve with a Rigid body. Set it back to Flexible. You can use a finer mesh in Modal.
After you solve the Modal, you can drag and drop a Transient Structural onto the solution cell of the Modal. Then you can apply an acceleration load to the Transient Structural to do the sine sweep for a Linear Modal Superposition Solution. No Large Deformation!
Paste the data from the attached text file, which is a 5g acceleration sweep from 20 Hz to 200 Hz sampled at 2000 Hz.
Analysis Settings, set the Time step to 5e-4 and Solve to get the Linear solution.
Duplicate the Transient Structural system and add the Fixed Supports, then you can turn on Large Deflection and perform the Full Transient solution.
You may as well add a Harmonic Analysis off the Modal to see what the frequency response is from the linear system.
Here is the Linear solution of the Transient Structural.
Thanks very much for your reply, you really help me a lot.
1. It seems that when I was doing the mode superposition by using the modal and transient structural, there is a limit for the time steps, I could not set it to 20000, instead the maximum I could put is 10000, do you have any idea why it will happen?
2. when I use the mode superposition with both the modal and harmonic response, there is a problem that I could not change the position where the acceleration applied from the whole body to the two surfaces on the two sides or corners, do you have any idea that how could I apply the acceleration on the two surfaces on the sides?
3. After I have done the full transient analysis, just insert the data I got into the matlab and deal the data with the FFT in matlab to get the frequency response. am I right?
4. one last thing is that: As for the BCs, we do have two choices like you stated before, either fixed support with acceleration or fixed rotation with displacement.
it does not matter which choice you pick but still will get to the same result at last. am I correct?
thanks very much again since you never feel impatient to answer my questions
Here is the Linear MSUP (red) and the Nonlinear Full Transient (green) deformation response vs. Time.
It seems the Linear had a lot more damping that the Full Transient. What data do you have about the damping in your PCB?
Also, you can see some of the nonlinear geometric effect that has stiffened the structure, leading to higher natural frequencies, leading to a later time when the resonance develops.
Now I will answer your questions.
1. Make the number of steps 1 and the End Time 10 seconds, make the Time Step 5e-4 seconds.
2. Acceleration applies to all bodies everywhere. There is no need to pick anything except one surface to point the acceleration vector. That is the Z-axis. Pick any surface for that.
3. If you put the data into matlab and do an FFT, you will get the frequency content in the data. There will be a big spike at the first natural frequency from the modal analysis, or near to there for the nonlinear case. That is not Frequency Response Function, which is a ratio of input to output.
4. You would have to try the transient structural both ways: fixed+tabular acceleration or fixed rotation+tabular displacement support. Note that you have to double integrate the acceleration signal to have a different table for the displacement.
Thanks for your very helpful reply.
1. In fact, I have not done ant damping test for the flexible PCB with IC chips, therefore, could I just assume a reasonable damping for my model? since there is two choices for the damping. (1) direct input (2) damping VS frequency. I have no idea how to use the setting of damping VS frequency. Instead I put a value to the direct input for the damping. could you please give me some advice? is it necessary that I have to test the damping from the experiment.
sorry that here are some of the information and questions that given from my major professor, could you please help me to answer it?
Here are a few comments:
1) Is it possible to apply force only to fixture, and not to the entire PCB simultaneously?
2) The FFT is a time-invariant technique, so it does not show nonlinear vibratory hysteresis. It is necessary to have the displacement data of the center of the PCB vs. time, so that it can be plotted against the displacement data of the chirp vs. time.
3) Is tabular displacement support a transient simulation?
4) As a different direction, is it possible to run a simulation at a particular frequency, then use the maximum displacement as the initial conditions for another simulation at a particular frequency? This should also work to find the vibratory hysteresis.
You will have to assume some value of damping. Since you are clamped so tightly to the PCB using a steel fixture and clamping bars, it is probably lightly damped. Try 5% damping. That means typing 0.05 in the Direct Input. There are experimental methods to measure the actual damping, like a pluck test.
1) In a Transient Structural, you are free to choose to apply a Force, Acceleration, Velocity or Displacement to the fixture. It is entirely up to you. These boundary conditions can be applied to the fixture that is bolted to the armature of the shaker, but if you use Force, then the mass of the fixture determines what the resulting acceleration is going to be. You can put the entire mass of the armature that drives the shaker table if you wish.
2) You can do a waterfall FFT and take blocks of data over the 10 second simulation and show how the frequency content shifts versus time.
You can output the displacement data of any point on the PCB or chip or fixture that you want. In a 3D model, where a chip stands above the PCB and there are lead lines coming out the side of the package and are bent down to be soldered into via in the PCB, then you can have motion of the chip separate from the motion of the PCB under the chip, but in your 2D model, that is simplified away into a single point.
3) Yes, you can have a Tabular input to the Displacement boundary condition that specifies the x, y, z coordinates of an edge or face vs. time.
4) In Transient Structural, you can run for a few seconds at a particular frequency, let a displacement amplitude develop, then change the frequency for the next few seconds. That is what we are doing in the Sine Sweep. Gradually changing the frequency from 20 to 200 Hz over 10 seconds.
Thanks very much for your help and reply.
1. I meet a convergence issue when I give the BCs as the fixed rotation and the displacement at the 2 surfaces on the corner(since that is my real BCs when I was running the experiment). I tried to change the iteration times from default 26 to 60, but it does not work and as for the command, I give the selection mode ALL, which is marked in black color on the following figures. besides I also upload the workbench file with it. thanks very much for your help
- All Categories
- Community Rules, Guidelines, and Tips
- News & Announcements
- Student Products
- Pre and Post Processing
- Physics Simulation
- Tutorials, Articles and Textbooks
- Installation and Licensing
- Student Competition Teams
- eMasters Degree from UPM
- Site Feedback
This Weeks High Earners
- 1 Need to help with dimension and changes, since it seems I am not able to do diff. in SpaceClaim 19.2
- 2 Ansys 19.2 student version installation problem
- 3 Wrong results for lift force every simulation
- 4 Installing the new version of License Manager
- 5 Another Work bench only opening a grey window [RESOLVED]