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Sir, based on analysis above, how to include progressive damage analysis? Please sir, it is due to my assignment.

Can I ask why did you define boundary condition for the bottom nodes in two different discpacement ? once you defined Z=0 and then add an other discpalacement condition for Y=3mm . I assumed we could define both in one displacement condition, is there any specific reason to divide it in two ? Thank you

i love you

This video just saved my life thanks, was very good.

what resin is the analysing done according to

Best please continue on making ANSYS complete CFD static structrual and CFX for the starters... also make videos regarding realtime problems as faced and solved with ansys

Very good and important for CLT and D matrix calcs.

Very useful application of composite plate buckling equation that has D11, D22 in it. This gives a hint that adding more plies or adding a core with increase the D (plate bending rigidity) values of layup.

whats the name of research paper you mentioned in video

Sir how we get the shear modulus (yz) value ?

Your way of explanation is very good 👌🏻

Amazing skills with Ansys Meric! WOW!

appreaciate your contiribution !!

I need you to help me with a model!! I need a guide with the step-by-step, im using the data of a article like you do in one of your videos, but in this case is different

how i am going to the same as thermal buckling

Hello, Thank you very much for sharing. I tried to apply the video exactly and when I try to apply the node selection at 13:53 minutes, I cannot get the same result. The same nodes are not selected. I wonder if it is because the Ansys version is different?

Hello please do you have experimental results that I can compare this current result with?

Teshekkur ederim, Meric bey. Cok yardimci bir video

Thank you Dr. Meric

Do you have a reference for your analytical equations that you could share?

Thank you very much!!What is that interesting testbook which you show from time to time?

very helpful, thank you

Please do more videos on Failure Analysis of Composite material plates using Ansys

sir please could you do more videos on testing of composite plates in Ansys such as Torsion test , Shear , Fatigue , Thermal , Fracture (crack) , Impact and how to model composite shaft in Ansys

very good😍

Thanks a lot for your wonderful video. I am following the tutorial to simulate laboratory testing on the rock. Is this possible to study the crack propagation in 2way coupling of structural and fluent? Regards,

Hello sir I have some doubts regarding fatigue analysis

Please refer us the text book you use for your study. It will be very useful to explore more topic

Hello sir, I am confised with material properties.. We have defined values for E11 and E22. Why is that we consider E33 to be same as E22? V12 is (epsilon y / epsilon x) when stress in x is applied We found V21 which is (epsilon x / epsilon y) when stress in y is applied. Why is it we consider in asys Poissons ratio YZ to be V21 = 0.0599?

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I followed your tutorial to practise stifferd plate structural modelling in ANSYS. Many thanks for the clear instructions.

Thank you very much, can you calcule this of the wind turbine.

If i wanted to the bussiness with you how can i contact you

I have a paid job for you

Thanks for your video In my case, i have to apply a frequency vibration 18 kHz at centre of the plate. Then find the vibration path of maximum peak to peak amplitude from center point to edge of the plate.

I liked the video, I am having a problem studying an assembly where one of the pieces is made of composite material. When placing the assembly in the ACP module, when I go to the setup only the part to which I am going to apply the composite material appears (I understand that it is because I defined it as a surface previously), but when I link the ACP module to the structural static I only see links the composite part and not the entire assembly.

Hello, thank you for your videos. But I have some questions about ACP. I am using ACP for my final project so I will put ACP in to the skin of the wing with woven material. And the interna structure just using general fiber. But when I try to do static structural analysis there so many error. That I don't know how to fix it. Maybe may you help me with that, so I can ask many questions more

Thank you, Meric!

Hello, can you help me ? So, I need to know how to simulate and study crack growth in bearing with ANSYS

Thank you for your video. When you apply the load, why you don't consider the edge length? As far as I know, the shell edge load should be divided by the edge length. Can you explain?

sorry, can i ask a question? how can i create a material with only E1, E2, v12 and G12? because in CLT plane element don't consider the direction of Z axial. i used ACP and transform to shell element, but if a change the value of G23, the result under torsion won't be the same? but i should be the same. why? can you help me? thanks. and 1:02 how comes the formula of v23, because i used this formula to verify any composite material from google, it's all wrong.

Hi, Thanks for the video!!!. Could you make a video on crack growth in Pipeline?

thank you very much, please i have question, how i can export this composite material from ACP to material data in Ansys

Hello Meric, I hope you are well. Your work has helped me a lot in a project. I have a question about the boundary conditions for this kind of materials, why should be considered as nodal displacement and nodal rotation and not use the option of "simply supported"?

Hi sir, can you conform loadfactor formula with reference.

You are very smart

Excellent analysis.

Thanks a lot. It was so useful, precise, and accurate.

Hello, thank you very much for this wonderful lecture. I have a question in the ANSYS program. I want to prepare, for example, a superimposed material in the form of a layer consisting of two materials, the first is fiber of any kind, and the other is a polymer material, with dimensions of 10 * 10 cm and a thickness of 2 cm. How do I calculate or how can I enter the volume fraction values For both subjects in the ANSYS program, for example, the first subject is 60% and the second subject is 40%. I hope you will help me in solving this problem. I mean, how can the volumetric fraction or weight ratios be calculated for each subject in the ANSYS program? With appreciation

Good Jobs, thank u sir...