Thermal Expansion   Thermal Gradient
11:38
Autodesk Nastran  Validation 2
16:21
3 жыл бұрын
Autodesk Fusion 360   Validation 2
14:03
Пікірлер
@keven-matthewlarrivee-font2678
@keven-matthewlarrivee-font2678 Ай бұрын
Hello Mike! Your videos have helped me a lot so far. I am trying to replicate simple hoop and longitudinal stress in a free cylinder with internal pressure. So far I've been able to make a 1/4 model of my cylinder, with symmetric constraints and an internal pressure. Compared with theoretical calculations, I am getting about 17% difference for axial growth and 5% on hoop stress. I feel these values are high. I am also unsure on how to get the longitudinal stress from Nastran. I've read Autodesk Material Orientation Doc but it did not help me much. I hope you can get back to me. The ultimate goal of this is to do structural analysis on cylone dust collectors.
@SameerHasan-c1i
@SameerHasan-c1i Жыл бұрын
Hi Mike... Thanks for this tutorial. For me it is a very helpful video. Could you please tell me how we can extract the bending and membrane stresses for shell elements in Inventor Nastran?
@MrJohanh80
@MrJohanh80 Жыл бұрын
Thanks so much for your videos. Greetings from Colombia.
@mikefiedler2039
@mikefiedler2039 Жыл бұрын
Glad you like them!
@OPrime9
@OPrime9 Жыл бұрын
Is there a way to print out a report showing what the thermal expansion values are, and the locations of the max/min deflections?
@mikefiedler2039
@mikefiedler2039 Жыл бұрын
Apologies for the late reply - but the answer to your question is yes. (1.) When you generate the report (right mouse click on Analysis in the Model Tree - Generate Report), presuming that you have Min/Max Markers turned on - when the program takes various images for the report, Displacement should be one of those images. The Min/Max markers should display location and value. (2a.) You can get all of the displacement values printed to the *.OUT file. If you double click on the analysis type (e.g. Linear Static) in the Model Tree, this should bring up the Analysis form. The default 'Output Options' pull-down you'll see is set to Plot by default. If you change that setting to Print, it will write all the displacements to the .out file. Note that if you have many nodes in the model, this can make for a very large out file. help.autodesk.com/view/NINCAD/2024/ENU/?guid=GUID-10BFD564-87F7-465B-B3BB-05F61E291DFA (2b.) If there is a smaller region of interest, it might be better to use the XY plot and select an edge of the geometry (for instance) or a few select nodes and then after plotting the values you can export that as a .csv file (which can open in Excel). help.autodesk.com/view/NINCAD/2024/ENU/?guid=GUID-3B982345-7F90-455E-894C-0B20F5D32A09
@gowthamshanmugam4290
@gowthamshanmugam4290 Жыл бұрын
How to apply temperature and pressure on same time for the storage tank
@juratomorad8641
@juratomorad8641 2 жыл бұрын
Thank you for a very informative video. You applied a temperature load on the inside surface, and on the outside surface. What temperatures does NASTRAN apply automatically to the surfaces on which no temperatures are applied? Is it T_REF? Or is it simply 0°C?
@mikefiedler2039
@mikefiedler2039 Жыл бұрын
Hello Jura! Because it is a steady state linear thermal analysis, the program is finding the thermal distribution after some 'infinite' amount of time, so the initial temperatures of the 'other' nodes does not matter because the lowest and highest temperatures in the model will be dictated by the loads that we did apply to the model and all other nodes will end up somewhere between those extremes. That said, two things to note (1.) if no load of any type is applied to a surface, the surface is treated as an adiabatic surface and (2.) the temperature of the other nodes would matter in a transient thermal analysis where we might want to see how fast something heats up or cools down. If it is a transient thermal analysis, then you would want to make sure that an initial temp is defined... this could be done with the 'initial condition' load with the 'sub type' of temperature - or first running a steady thermal to get the starting distribution for the transient analysis. I'll make sure to get to some transient thermal analysis as an example.
@juratomorad8641
@juratomorad8641 Жыл бұрын
@@mikefiedler2039 Thank you for a clear explanation!
@zeinabashtab1456
@zeinabashtab1456 2 жыл бұрын
Hi. Can you please let me know the name of the software that you have used in this video to draw a figure of a torus? Thank you.
@mikefiedler2039
@mikefiedler2039 2 жыл бұрын
Hello Zeinab. This geometry was constructed in Autodesk Fusion 360. The Fusion 360 product has cad modeling abilities along with simulation, drawing creation, rendering and more. You can find more information about that product here www.autodesk.com/products/fusion-360/overview?term=1-YEAR&tab=subscription Disclosure: While these videos are done in my leisure to help educate and promote the use of FEA, they are not officially part of Autodesk formal learning content - though I am an Autodesk employee. Thanks for watching!
@pablobegazzo7596
@pablobegazzo7596 2 жыл бұрын
gracias por la buena explicacion
@leonpowers8543
@leonpowers8543 2 жыл бұрын
ᑭᖇOᗰOᔕᗰ
@HAN-kh9qk
@HAN-kh9qk 3 жыл бұрын
nice tutorial! thanks
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
You're welcome!
@lucmartz
@lucmartz 3 жыл бұрын
Thanks for this video, very clear explanation!!
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
You are welcome!
@navalfa7291
@navalfa7291 3 жыл бұрын
Thanks Mike. I work for a company that makes pressure vessels and heat exchangers. Historically we used to use Abaqus for our stress analysis. But due to budget constraints, we are moving to Inventor Nastran as the only FEA option. Your videos are great help for me in making that shift.
@navalfa7291
@navalfa7291 3 жыл бұрын
Is there any reason you only applied Z sym only on the bottom of the cylinder instead of both top and bottom? I can see some gradient difference in your displacement plot at 6:41.
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
Hello Adil Apha - thanks for watching the video! So, the z symmetry constraint (or Tz) constraint is really there just added at one end of the model to keep the model statically stable - but I don't want to over constrain the model. To apply the z constraint at the opposite end would restrict any axial expansion or contraction that might happen in the model due to the loading. When we look at one of the radial directions, we do expect it to be a non-gradient result (e.g. same at the top and bottom)... but right, since I didn't control that growth or contraction, the model does experience about .0015" of axial contraction. So, at the 6:41 mark in the video, what is displayed is total displacement - or a combination of the x, y and z components - and because of that difference in the z results, we get the gradient. Good observation, hopefully that explanation makes sense to you. In short though - ultimately the most important thing is trying to make sure that your constraints match the 'real world' as much as possible when it comes time to perform your analysis... and good to observe how the decisions to apply (or not apply) particular constraints influence those results. Take care!
@navalfa7291
@navalfa7291 3 жыл бұрын
@@mikefiedler2039 Understood. Thank you for your detailed response.
@CJR789
@CJR789 3 жыл бұрын
i''m absolutely beginner thanks you very much for posting this video, this really help me to learn...
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
You're very welcome!
@ivanildo5891
@ivanildo5891 3 жыл бұрын
Excelente!
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
Thank you for watching!
@navaneethv1709
@navaneethv1709 3 жыл бұрын
Thanks Mike.
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
Certainly! Thank you for watching!
@navalfa7291
@navalfa7291 3 жыл бұрын
Thanks very much.
@navalfa7291
@navalfa7291 3 жыл бұрын
I think the result might change if instead of selecting the full face for a fixed constraint and we selected just the lower bottom edge of the bar fixed. One reason why many get different results. Anyway, nice video.
@navalfa7291
@navalfa7291 3 жыл бұрын
Nice video. Thanks. just a comment. This 5th edition of Roark and Young is one of the hardest editions to find online for purchase. Only 7th and 9th editions are available on amazon.
@navalfa7291
@navalfa7291 3 жыл бұрын
This is what i was looking for.
@navalfa7291
@navalfa7291 3 жыл бұрын
Nice video. Thanks for sharing.
@navalfa7291
@navalfa7291 3 жыл бұрын
excellent video thank you. Newbie to inventor nastran here. is there anyway to constrain axially by defining an axis?
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
Hello. Thanks for watching! In reply to your question, 2 different ways to possibly approach this; 1. When adding the constraint, note that 'Constraints' is a pull-down menu. If you change it to 'Pin", then you can apply constraints to be able to fix (or not fix) the radial, axial, and tangential directions. Note this must be applied to cylindrical faces. 2. Otherwise, further down the Model Tree, you should see an entry labeled 'Coordinate System'. There you can define other rectangular, cylindrical and spherical local coordinate systems. The newly defined coordinate systems can then be used when applying either constraints or loads on the model. Applying: knowledge.autodesk.com/support/inventor-nastran/learn-explore/caas/CloudHelp/cloudhelp/2019/ENU/NINCAD-UsersGuide/files/GUID-EB94687D-45AE-4A43-9BFF-6B367E4B59A6-htm.html Using the lcs: knowledge.autodesk.com/support/inventor-nastran/troubleshooting/caas/sfdcarticles/sfdcarticles/How-to-visualize-the-coordinate-system-in-Inventor-Nastran.html.
@navalfa7291
@navalfa7291 3 жыл бұрын
@@mikefiedler2039 Thank you.
@navalfa7291
@navalfa7291 3 жыл бұрын
1. When I tried doing the pin constraint, the solver came up with the fatal error "FATAL ERROR "E5000: SINGULARITY DETECTED". The model is very similar to that you have in the video.
@mikefiedler2039
@mikefiedler2039 3 жыл бұрын
@@navalfa7291 Constraints are a fairly common source of that issue. So, you indicated that you were using some pin constraints. Imagine you only constrain the tangential direction on a cylinder. If the loading should cause the model, as a whole, to (for example) translate axially, that would lead to it being statically unstable and end with that error. You should try and ensure that all possible directions of motion are accounted for in some way in a linear static stress model. The simple test to see if that is the source of the error would be to just add a fully fixed constraint somewhere on the part, try and run it again and see if that fixes it. If so, then you can remove the fully fixed constraint and try to apply something more appropriate. Material properties are another source of this error message. You should take a look at the material properties and make sure that all have a reasonable modulus of elasticity and Poisson's ration. If you have gravity or any other type of acceleration, make sure you also have an appropriate material density. The help page for this error message is here; knowledge.autodesk.com/support/inventor-nastran/troubleshooting/caas/sfdcarticles/sfdcarticles/FATAL-ERROR-E5000-in-Nastran-Analysis.html#:~:text=If%20the%20problem%20is%20caused,low)%20values%20in%20material%20properties.&text=If%20G3005%20warnings%20occur%20in,or%20using%20a%20finer%20mesh.