Відео

Hello what are the software’s required for this work all software which you have used in this video please tell me

how and where can i get the tyre geometry

can you tell me the name and mode of your system?

Is there a way to have fluent output the air exchange effectiveness value rather than having to use a separate calculator program? I would like to make a contour plot that shows air exchange effectiveness. Right now I am only able to make a contour plot that shows age of air.

please share the wing design

how to design the wing of this aircraft.

permission, where is the place to download the geometry

link download geometry is expired

I have a question. When you click "Sizing" and then under "Definition" i don't have "Body of Infuence". What should i do?

Very well benefit of this , thx sir 👍🏻

sir can you please do airfoil with flap :)

In this how to find the cd and cl of the tyre..?

Why did you include the UDS, after the velocity at the outlet, converged? Does it not work if you include the UDS from the start? Thank you

Promo_SM 😣

I find the cd values to low with slang angle 80 degree I changed just chamber part in design modeler, I have used same mesh but cd is coming 0.28 it is too low with this slant angle how ı can change?

Waiting for the next part

amazing!!! Thank you so much for sharing this!!!!!!!!!

Hi thanks for this.

Thx for sharing sir 🤝🏻

Great job

Hi Sir, how can I set an other AoA? We have only farfield module. Is it possible to set an X and Y velocity value?

The drag coefficient is too low?

Thanks for this tutorial. I didn't understand one part. How did you manage to set x axis starting from 0 to 1 or default setting is like this?

mine gets stuck on "attaching to assembly" ?

In our work, the density is constant. So the source of mean air age will be constant everywhere. Kindly explain..

this was super helpful thank you!!

Great tutorial! One thing I don't understand is why we used a pressure solver rather than a density solver in compressible flow

Can I get 4 instead of 36 in setup? does this cause a problem? I can't run it because I'm a student licensed.

Inflation and face mesh are closing each other, what kind of way should be followed to solve this? I want to give inflation to my airfoil, for this I found my first layer thickness value, but the inflation is not given on top of the operations you have done, what is the reason? I am getting invalid method error.

How did you calculate the value of area?? If my cylinder is of D diameter what should be the area in D???

Create an unstructured mesh of Gable low-rise building (Convert to Polyhedral mesh) ua-cam.com/video/UFW-ISTEHq0/v-deo.html

Create an unstructured mesh of Gable low-rise building (Convert to Polyhedral mesh) ua-cam.com/video/UFW-ISTEHq0/v-deo.html

Hello, sir.. This is my final year project, thanks for the video as it has helped me a lot, I am facing an issue in setup, it is showing *divergence detected in amg solver... *, Can you please suggest how to get rid of the error

The first layer height in your video is 0.4mm, but it should be 0.04mm or less if you want the y+ value to be around 30,right?

After building this, is it possible to do a cavitation analysis of it

hi everyone, who can make rans and urans simulation of Ahmed body with discrete adjoint optimization?

Next part

Where is IFSTREAM?

The drag coefficient should be around 1.3 for Re= 100

Excellent tutorial, one of the greatest actually.

Kindly tell what you did between 10 35 minutes and 10 45 minutes?

How long do you run the simulation?

Soooo much click click to analyze a single airfoil !!! at one angle of attack !! .. NOPE

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what if uref is changing over time in a transient simulation? how can we do this in the udf? pls any advice

what if uref is changing over time in a transient simulation? how can we do this in the udf? pls help

says failed to process a boi, boi either too thin or open? can you help me with this

Plz bring more lectures

Sir, how can i contact you?

There is considerable error in the cd value