Why max. Stress is not 3 times the applied pressure, as per the stress concentration factor.

Thanks!!!!!!!

Again great work Ismail

Thank you for this

Nice 👍

Thanks!!!!!!!!!

Thank you , it was vwry helpful!

why you took time period as 0.25 and you assigned speed as 0.2 meter per sec and tool length is 0.2 whats the reason, i am not able to get it, if you could explain

what software is this using?

i don’t get the result tho

Degree of freedom 11 and at least one of degrees of freedom 1 thru 6 must be active in the model for *dynamic temp-disp. Check the procedure and element types used in this model. Analysis Input File Processor exited with an error. How To Solve ABove Error anyone have Idea ?

How do you calculate displacement at failure in damage evolution

Merhaba Hocam sizinle nasil iletisime gecebilirim? Projemle ilgili sormak istedigim bazi sorular var. Yardimci olursaniz cok mutlu olurum.

Very nice. Thank you for sharing.

For anyone trying to follow along like me / skipping around a lot and checking: 0:00 Creating the Beam 0:35 Partitioning the Beam 1:44 Creating the Crack 2:18 Creating the Load 2:58 Creating the Assembly 5:02 Adding Material Properties 5:32 Section Manager for Material for Parts 5:53 Creating the Steps 6:31 Setting up General Solution Controls 6:56 Setting Interactions 7:25 Setting the Crack 7:47 Crack Interactions 8:00 Load Boundary Conditions 8:45 Creating the Mesh 9:27 Setting the Job 10:03 Visualization Thank you for setting this up, helped me learn a bit about abaqus!

how do you change the stl file?

Hello sir ye load ek sath all surfaces pe kese select Kiya

Hi. Could you try to help a structure like Miura Origami based? Thanks

❤❤

How the tabulated plastic properties for the steel bolts are taken ??? any specific equation you can suggest

سلام ، بارك الله فيك شكرا على هذا الشرح المبسط ، اذا امكن هل يمكنك مساعدتي؟ اريد automatisé l'essai de traction avec un script python و وجدت صعوبات

Hey can you do a 3-point bending test with a sanwich structure that has a core and on top and bottom a composite layup. I have to do this and I don’t get it. It should be dynamic explicit because it has to break after a certain pressure from the top. Left and right is a support and one on the top the pressure comes forme the top. I hope you or someone can help me

What input do we have to give to determine the breakout point of steel

How to get the fracture of the material without giving crack initially

How to determine the Penalty friction coefficient for different materials?

BC

hi, Thanks for your video, please what dimensions did u use?

But it's loosing all the details... How to preserve the details while the process???

Please send your contact details

I am research scholar and I need your help in my research work

Hi sir

not audible.

Hello, I am performing a FE analysis in ABAQUS and I have some issues regarding thermal simulation, may I get your help to solve some doubs?

Hello. Thanks for the video. Where can I find the material properties, especially the damage evolution and stabilization that you used?

pops

Thanks for your video... But i have run it in the abaqus.. But i am unable to complete my analysis.. Can you please help me with this

Are there any scientific publications on which this video is based?

thank you sir for this video,can you please send me this data

Can u provide the material properties of concrete

Please how can i model a spiral stirrup as wire in abaqus

Is there other option if extended tools are not working

Can I get this model?

Oh wow, it's really cool. But what is the mesh size for this? Below ~1mm?

I tried the similar model but using the viscoelastic material. Although I set the Poisson's ratio 0.48， the results the volume of the ball has decreased, and U2 and U3 perpendicular to the compression direction are almost equal to zero. What is the reason for this?

How to simulate for dissimilar material loke dissimilar welding. How to choose dissimilar material in two end

How to simulate for Dissimilar material like stainless steel inconel material

For plotting the load slip respmse im not getting its in a proper way what can i do

how can i assgin a element section properties for this kind of discrete rigid body in abaqus?

Hello sir you are great i enjoyed a lot while watching this tutorial thank you so much