Ansystant

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@CleitonLimaBoeno 6 күн бұрын

Very intersting your design method.

@Flodar_Eltih 21 күн бұрын

World’s worst software ui. Its like halving an atom.

@ruslansabah4070 29 күн бұрын

Can you make simulation for this vedio

@ernestjesly Ай бұрын

What should be the reference area for analysing the whole aircraft?

@AjayRahul-be7mr 2 ай бұрын

The steps u did from 12:40, that is from output mesh; is it necessary or can we save without it??

@bradd8841 2 ай бұрын

Thank you for your input, well made video.

@poorvamondal1977 2 ай бұрын

I have taken vapour volume fraction as 0 but in solution not getting any contour for volume fraction. Why?

@muhammadwaseem-xm2co 2 ай бұрын

Hello sir, I have a hexahedral multi-block structured mesh in ICEM CFD, I got some results from this mesh. Now, I have to do a mesh independence test. Please tell me which is the correct way to increase the number of mesh elements: Should I 1) Re-mesh the whole geometry with smaller element size 2) increase the number of nodes in each block. 3) increase the scale factor like 1.2 or 1.3 etc.... Thank you!

@anasbataineh2644 2 ай бұрын

hello, i want to mesh a hollow 3d nose cone. Unfortunately it doesn't work with this method, please help.

@designsandsimulations887 3 ай бұрын

I want to design an ICEM mesh for a NACA 0012 airfoil wing with waviness over the leading edge.

@matthelord7695 3 ай бұрын

That is insanely innacurate

@jeevanshrao2471 3 ай бұрын

Ansys gives the warning that you cannot use pressure farfield for non ideal gas and until that BC is changed setup cannot be initialized. How did you get results??

@Ansystant 3 ай бұрын

Air was modelled as an ideal gas in this simulation. You can also use zero shear wall boundary condition.

@Pa5word 3 ай бұрын

best channel name ever

@marouaneelalaoui8999 3 ай бұрын

Thank you for this video 🫡

@boowboow311 4 ай бұрын

hello, can you tell me your reynold number's value?

@kemalsorucuoglu3689 4 ай бұрын

thank you

@user-el9mv9wp1q 4 ай бұрын

Thank you so much Sir. can i have your email address please

@ozgunonen7427 5 ай бұрын

excellent job

@KhalilKhalil-dv2hw 5 ай бұрын

Please I want to ask if we are able to add an inflation layer around the wing using this type of mesh ?

@goktanyldrm9028 5 ай бұрын

thx sir for ur unique video

@maryambouftih814 5 ай бұрын

Hi! Can I have this structure for practicing more

@taharchehat9333 5 ай бұрын

How can we do it with Fairfield it doesn't work with me

@madansridhar924 6 ай бұрын

Hii can u make a video for multi element airfoil?

@lilial730 6 ай бұрын

how calculate first cell height in prism layer in convergent-divergent nozzle!!!!!

@saurabhchhipa1062 6 ай бұрын

Sir i need your help , will you help me in meshing

@anaritalourenco9472 6 ай бұрын

Hello, everything is fine? I hope so. How did you conclude that the structure was safe? I don't understand the safety factor analysis, can you help me, please? I'll be waiting for your response and if I can help somehow, let me know how. Thank you, continued success!

@ayubadnan6815 6 ай бұрын

❤❤

@marcellveres4588 7 ай бұрын

Hello! I have a problem with cylindrical support, when I select the face it doesn't work. I don't know what could be the problem, maybe there is a limit on student version, or because it is an .iges file from solidworks Somewhere I saw that I have to select proximity and curvature, but the choosable only the Yes or No. Can anybody help me?

@mihailanga7352 7 ай бұрын

Great tutorial about meshing! Can we have one based on imported geometry?

@ethanmax97 7 ай бұрын

Nice mesh, were you able to save it, I always get the error when I convert to unstructured mesh and save it to try and import for ansys fluent

@khaihoangcao9606 8 ай бұрын

Hello, do you mind if I have a question to ask you? To mesh, we have to divide the solid into parts. So when adding the next model, how will we have to set up the connection, or will the application automatically understand that they are still tied together? Thank you.

@Ansystant 8 ай бұрын

They bodies that are grouped as a single "part" in geometry do not need any connections. The software already knows that it is the same part (tied together). For multiple parts, you make connections between them. E.g. if you have a nut and a bolt (2 parts total), you will make a connection between them. But you do not need to make any connection between the different bodies of bolt (if you split the bolt in multiple parts in designModeler to get a good mesh)

@sintonghutabarat9215 8 ай бұрын

can i ask ur text books validation?

@baqeralzaki9234 9 ай бұрын

nice videos. Please add the gemo and please make more of these videos

@baqeralzaki9234 9 ай бұрын

What a great tutorial. Thank you

@서지완학생공과대학기 10 ай бұрын

Hello In 2D, i stretch depth 1m to 2m. Does frontal area double in size? i want to know relationship between depth and area in 2D reference value. Thanks :)

@AlloyedFrequencies 11 ай бұрын

awesome thank you

@ammarlaichi8474 Жыл бұрын

You are perfect job; you are beautiful, I want to create mesh using ICEM because I found it gives a good mesh then others, can you help me?

@alexua45 Жыл бұрын

Can you please help me to mesh my model using ICEM-CFD?

@Ansystant Жыл бұрын

You may contact us at Upwork: www.upwork.com/freelancers/~01c3dbc915cd800047

@pavankarthik9395 Жыл бұрын

Everything is fine but, whenever I am trying to make a new part, it is not showing as sweepable bodies, which was shown earlier

@christosvasiliou219 Жыл бұрын

i love you

@gagandeepsingh1173 Жыл бұрын

9:47 does a time skip, you clear a warning by ansys. I want to know how cause im facing similar warning.

@alexanderwicke9920 Жыл бұрын

It’s the best video to show how to meshing

@alvaromfo Жыл бұрын

I'm working on a 3D semi tapered wing analysis using Fluent Aero, and I'm setting up the value of the root chord as the reference length, but, since it's not a constant chord wing, should I use the value of the mean aerodynamic chord instead?

@zhaoguoqing Жыл бұрын

Great viedo.

@611538 Жыл бұрын

Don't split mesh and you will have better mesh with multizone method

@Ansystant Жыл бұрын

Maybe yes. But this tutorial is more focused on learning sweeping methods and meshing techniques.

@nicolamenga8943 Жыл бұрын

Hello. Thank you for the video. I have a question. In the tab of the reference values there are two further spaces: the "Compute from" and the "Reference zone", for which a part of the geometry can be selected. How can I set these information? Thank you.

@Ansystant Жыл бұрын

"Compute from" option is used to calculate reference values automatically based on a selection (e.g. using value of velocity at inlet as reference value). You can also manually enter the values. The option is just there for ease. Reference zone selection becomes important when you are dealing with problems having multiple frames of references. If your problem only has a single FOR, you don't need to select any.

@nicolamenga8943 Жыл бұрын

@@Ansystant Ok, so I can set the reference values without to set the "Compute from" information. Before seeing your video I only set the "Compute from" to the "Inlet" (velocity inlet). In fact, I was getting very wrong value of cl and cd. This video is very useful. Thank you.

@Ansystant Жыл бұрын

Glad we could be of help.

@MaraAmaraaaa Жыл бұрын

Pinis

@amitkumar-kw1eo Жыл бұрын

Nice video, Thanks for sharing. Could you tell me, why the cubical flow domain is used and not spherical to get o grid? Thanks..

@neovo903 Жыл бұрын

I tried this and it doesn't work. Next to the Face Meshing Icon there is a small blue stop sign instead of a green tick

@ShivaRam-yn6ed Жыл бұрын

Only a person who knows the difficulty of ICEM will appreciate this video. Thanks for the tip.

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