Where can I find the CBUSH Connerections in FEMAP 2401 ?

nice video, thanks for posting

Oh my god, this is a great webinar!

How did you do that middle selection at @38:00? Are there any other type of selection features like that we should know about? Thank you.

is there a way to generate Aero Panels which fit the wing surface?

Thank you!, please can you share the test file which you shown in this video

GOSTOSO

Does this work for supersonic/hypersonic velocities? I don't see an option for using Piston theory anywhere.

But how do you setup the contact? I'm having a problem with it

Shame that Siemens stopped supporting ADINA out of the box!

Why grav card doesn't work. So it doesn't matter on which planet you are flying according to this. Please can anybody answer

excellent freebody demo.

Hi, Thanks for great Video! To use python interface with femap as explained above, one should open femap GUI first to see the connection (if I am right!). How one can simply run femap GUI from python? Thanks

Excellent info on freebodies

Hey! This is an absolutely amazing simulation! Would there be any way to get codes or project for it, to change structure and variables for a project on flutter I'm working on.

Great video. What I would love to see is a video of complete part. What I mean is that in this demo you have two core ply's but you never covered it with "overcore" ply's and what goes into doing it. Also it would be great if you could show generating 3D solids out of finished part that could be evaluated in the assembly (wherever this parts is intended to be used). Another important thing would be to demonstrate how fibersim data could be exported to FEA packages - part with resultant (result of manufacturability simulations) ply's, fiber orientations, etc. That would give the full picture of fibersim being used in composite design and manufacturing.

Pretty cool. I’m a senior at Embry-Riddle, so it was a fun fact to hear the presenter is an alumni. Go Eagles!

why did he multipl mass by acceleration? that gives newtons! (or whatever american version that would be) shouldnt mass just be the lbs?

Why a software in 2021 hasn't undo feature?

The video is desyncred with the audio, 1 minute of lateness

Thank you very much for this video, it helped me understand PSD analysis quite a bit!

Very solid video. Much appreciated!

Need yourself a mic, audio is terrible

If the purpose of fillets is to reduce stress concentration, why is FEMAP designed to analyze without these fillets? Wouldn't that give high stresses at midplane intersection joints?

Hey there. I need to perform similar simulation by not on aero body. Can i do it using these steps. My body is cantilevered tube in an air flow.

Thanks!

Is it possible to try a demo of this tool? In the Siemens website there are few information about it and how eventually request a demo. Thank you in advance

thanks

Please make more advanced tutorial on beam analysis!

Hi,there. What confuses me is how to link the webs with the spar. Since I only have the outer shape of the wind blade, all layers must be stacked inward. And that makes the t-linking look weird. The shell element totally immersed the first row of web elements. Does that work?

nicely explained and demonstrated.

Great video. Could I just ask if I can find somewhere the cad to try myself fibersim on the same project? secondly, how did you draw the net/boundary curve and the core's curves? project curve? Thanks

been able to do the analysis finally, but still unable to get the flutter animation for velocity where damping becomes positive, can u please help me with that. flutter preview thingie u mentioned is not working please

Great webinar!

I just used data surfaces for the first time about a month ago. Thanks for the video!

m trying to practice this rigid trim and rigid trim off and m facing the same problem u did mention. even when m editing the trim card as suggested by you. whenever i recheck it, just to confirm that 1 against pops up. and my results are also the same. means rigid trim.onnd off deformationis exactly the same. please can you help me wirh how did manage tomitigate it

I really wish they would finally develop a better post processing for random vibe.

How to find these warning and limit angles of a prepreg, is there any tests for those

Hello and thank you for posting this content. May I ask what source you are referencing for the stiffness properties when defining the material. Thank you.

Thank you a million! Very helpful!

Thank you for a good introduction webinar :) Yet I believe that it can be improved: unfortunately there are small topics left untouched and uncovered - like really basic 3D-CAD operations (just few minutes on defeaturing and automated flow volume extraction would be enough), getting a bit deeper to the concept of Parts (Surfaces) -> Regions (Boundaries) workflow, meshing of a simple geometry (maybe with 1 surface control for refinement), monitoring quantites and running the solver, post-processing just as couple of scenes.

Great video! Is there a way to share the cbush api or a tutorial on creating one? Thanks

Great tutorial! Where we can find the cbush conneciton api? Or a guide on how to create one! Thanks

Is there the possibility of getting the API code for the CBUSH connection? I would be very pleased. Thanks :)

Proud to work with FEMAP <3 <3 <3

Excelent! THANK YOU A LOT!

Video is about 1min20sec ahead of the sound

Jay, that was very helpful - thanks!

I always enjoy when yall post videos. There's always new techniques to use, and I appreciate your team's willingness to discuss.

Great video! But how can I properly select structural nodes in order to have a spline that correclty transfer aero model to strucutral model? Which nodes should I choose?