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Meric Büyükkoyuncu
Registrace 13. 09. 2014
SMART Crack Growth Analysis ANSYS 2020R2
Static SMART Crack Growth Analysis ANSYS 2020R2
Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165
Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165
zhlédnutí: 32 540
Video
Buckling Analysis of Composite Plates Ansys ACP Tutorial (Theory and Calculations are Explained)
zhlédnutí 11KPřed 3 lety
Buckling Analysis of Composite Plates tutorial by ANSYS 2020. Theory and the analytical calculations are shown. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165
Bending of Composite Plates ANSYS ACP Tutorial (Analytical Calculations are Shown)
zhlédnutí 9KPřed 3 lety
Analytical calculations of Bending of Composite Plates are shown in the video. Also Bending conditions is modelled in ansys by using ACP Tool. Analysis is validated according to the analytical calculations. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Other videos: czcams.com/video/SHqUajOzEMg/video.html czcams.com/video/rsznfujPKac/video.html czcams.com/video/GE0NycSvVmI/video.ht...
How to Write a Matlab Code for Composites (D value/Bending/Buckling/Vibration Calculation Code)
zhlédnutí 12KPřed 3 lety
Writing the matlab code for laminated composite plates to calculate "D" value, bending deformation, critical buckling load and natural frequency. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Other videos: czcams.com/video/SHqUajOzEMg/video.html czcams.com/video/rsznfujPKac/video.html czcams.com/video/GE0NycSvVmI/video.html czcams.com/video/2HPEPTdnupM/video.html czcams.com/video/p...
Modal Analysis of Composite Plate Ansys 2020 ACP TOOL (Analytical Calculations and Theory Explained)
zhlédnutí 21KPřed 3 lety
Natural frequency analysis of laminated composite plate in ANSYS 2020. Analytical calculations and theory are explained. ANSYS results are compared with the analytical calculations. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Other videos: czcams.com/video/SHqUajOzEMg/video.html czcams.com/video/rsznfujPKac/video.html czcams.com/video/GE0NycSvVmI/video.html czcams.com/video/2HPEP...
Flexural Stiffness Calculation Tutorial In Composite Plates (D Value)
zhlédnutí 3,7KPřed 3 lety
Calculation of flexural stiffness of laminated composite plates. Also, importance of D value and D matrix are explained. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Other videos: czcams.com/video/SHqUajOzEMg/video.html czcams.com/video/rsznfujPKac/video.html czcams.com/video/GE0NycSvVmI/video.html czcams.com/video/2HPEPTdnupM/video.html czcams.com/video/p_EbVknef9w/video.html czc...
Modal Analysis of PLate in Ansys 19 (Natural Frequency, Resonance, Vibration)
zhlédnutí 19KPřed 3 lety
Modal Analysis of PLate in Ansys 19. Also, natural frequency and resonance are explained. Analytical calculations of the natural frequency of the plate are compared to Ansys results. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Other videos: czcams.com/video/SHqUajOzEMg/video.html czcams.com/video/rsznfujPKac/video.html czcams.com/video/GE0NycSvVmI/video.html czcams.com/video/2HPE...
Linear Buckling Analysis Ansys 19 ( Analytical Calculations and Theory are Explained)
zhlédnutí 11KPřed 3 lety
Linear Plate Buckling Analysis by Using Ansys. I did analytical calculations for the plate and I explained the theory. Also, I validated analytical results with the ansys Eigen-Value buckling analysis. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 The other videos: czcams.com/video/SHqUajOzEMg/video.html czcams.com/video/rsznfujPKac/video.html czcams.com/video/GE0NycSvVmI/video.htm...
ANSYS Nonlinear Buckling Analysis of Stiffened Plate (Johnson-Cook-Power Law Plasticity)
zhlédnutí 6KPřed 3 lety
Validation of Nonlinear Buckling Analysis of Sub-stiffened Plate by using Johnson-Cook and Power Law Plasticity Data in Ansys 19 Excel File of Plasticity Data: dosya.co/naw9y5a91siq/Aluminum_2024-T351.xlsx.html Linkedin:www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Other Videos: czcams.com/video/rsznfujPKac/video.html czcams.com/video/GE0NycSvVmI/video.html czcams.com/video/2HPEPTdnupM/video...
Optimization of Stiffened Plates Against Buckling ( Optimization Tool Ansys 19)
zhlédnutí 6KPřed 3 lety
New tutorial is about optimization of stiffened plate under buckling loads. In this tutorial, height and thicknesses are considered during optimization process. If you are curious to see, please watch the video and comment. Linkedin: www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Another Videos: czcams.com/video/GE0NycSvVmI/video.html czcams.com/video/2HPEPTdnupM/video.html
Nonlinear Buckling Analysis of Stiffened Plates (ANSYS 2020)
zhlédnutí 20KPřed 4 lety
Nonlinear Buckling Analysis of Stiffened Plate compared to the Article Results. Linkedin Account : www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Article Link: drive.google.com/file/d/1lWitoGUCNtWHDxy771eYxHcKm6KFXMh6/view?usp=sharing Another Analysis: czcams.com/video/2HPEPTdnupM/video.html
Linear Buckling Analysis of a Plate By Using ANSYS 19 (Türkçe)
zhlédnutí 2KPřed 4 lety
Merhabalar, ben makina mühendisi Meriç Büyükkoyuncu, Ansys 19 ile ince plakaların lineer buckling analizini yaptım ve bu analizimi analitik formül çözümü ile kontrol ettim umarım beğenirsiniz. Video ile ilgili sorularınızı ve önerilerinizi yorumlardan bildirebilirsiniz. Linkedin : www.linkedin.com/in/meriç-büyükkoyuncu-10b831165 Referans: ocw.mit.edu/courses/mechanical-engineering/2-080j-struct...
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?
Hi, did you solve that issue
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?
Meriç bey linkedin üzerinden iletişime geçtim . Rica etsem dönüş sağlayabilir misiniz? Teşekkürler
Meric Bey merhaba mail adresinizi paylaşma şansınız var mıdır ? Sizinle İletişime geçmek istiyorum.
Merhabalar, linkedin üzerinden geçebilirsiniz
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...
Thank you for your efforts
do you have the code to find yeild stress and plastic strain on matlab?
Professor can you tell me what would be the equation of frequency of a beam under dynamic load?
Hello, thank you for your great video. I have a question: what you call "fracture toughness", it is rather the "threshold stress intensity factor" right? Bevause your crack did not grow for SIF value below the value you enter in Ansys ("Critical rate")
Hello, can you pls identify the material names used in this video. Thanks.
why can't you give the code
How to do effect of ultraviolet radiation in ansys?
Hello sir, Is there an any way that you can share the Johson-Cook pdf?
hi meric, could you compare the external force = first natural frequency to form a resonance i am interested to see the failure of the plate .please guide me