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Introduction To CFD
Добавлен 31 май 2018
Official channel of video tutorials for "Introduction to CFD" class of Dr A.Nejati At SRBIAU...
TA : M.Davoodi Mehr
TA : M.Davoodi Mehr
Axial Turbine Blade with Periodic Boundary Meshing in Gambit
Introduction To CFD
Dr A.Nejati
TA : Maziar Davoodi Mehr
Aerospace Department
SRBIAU
Dr A.Nejati
TA : Maziar Davoodi Mehr
Aerospace Department
SRBIAU
Просмотров: 2 104
Видео
Velocity Contour Animation of Rotating NASA SC-20612 AIRFOIL - Realizable k-e Transient
Просмотров 3696 лет назад
Rotation Speed : -0.4 rad/s Flow Time : 1s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Pressure Contour Animation of Rotating NASA SC-20612 AIRFOIL - Realizable k-e Transient
Просмотров 6246 лет назад
Rotation Speed : -0.4 rad/s Flow Time : 1s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Local Eddy Viscosity Contour in Farfield Animation of NASA SC-20612 AIRFOIL - DES Transient
Просмотров 816 лет назад
AOA = 10 Flow Time : 2s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Local Eddy Viscosity Contour Animation of NASA SC-20612 AIRFOIL - DES Transient
Просмотров 1406 лет назад
AOA = 10 Flow Time : 2s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Global Eddy Viscosity Contour in Farfield Animation of NASA SC-20612 AIRFOIL - DES Transient
Просмотров 186 лет назад
AOA = 10 Flow Time : 2s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Global Eddy Viscosity Contour Animation of NASA SC-20612 AIRFOIL - DES Transient
Просмотров 1056 лет назад
AOA = 10 Flow Time : 2s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Velocity Contour Animation of NASA SC-20612 AIRFOIL - DES Transient
Просмотров 1606 лет назад
AOA = 10 Flow Time : 2s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Pressure Contour Animation of NASA SC-20612 AIRFOIL - DES Transient
Просмотров 1106 лет назад
AOA = 10 Flow Time : 2s Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Flow over a Cylinder Transient SST - Eddy Viscosity Animation
Просмотров 9296 лет назад
Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Flow over a Cylinder Transient SST - StreamLines Animation
Просмотров 1576 лет назад
Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Flow over a Cylinder Transient SST - Velocity Vectors Animation
Просмотров 676 лет назад
Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Flow over a Cylinder Transient SST - Velocity Contour Animation
Просмотров 426 лет назад
Introduction To CFD Dr A.Nejati TA : Maziar Davoodi Mehr Aerospace Department SRBIAU
Flow over a Cylinder Transient SST - Pressure Contour Animation
Просмотров 2226 лет назад
Flow over a Cylinder Transient SST - Pressure Contour Animation
Laminar Steady and Transient with SST Flow Over a Cylinder analysis in ANSYS FLUENT 18.2
Просмотров 18 тыс.6 лет назад
Laminar Steady and Transient with SST Flow Over a Cylinder analysis in ANSYS FLUENT 18.2
2D Lid Driven Cavity Laminar Flow analysis in ANSYS FLUENT 18.2
Просмотров 2,2 тыс.6 лет назад
2D Lid Driven Cavity Laminar Flow analysis in ANSYS FLUENT 18.2
2D Lid Driven Cavity Analysis in Fluent 6.3
Просмотров 5766 лет назад
2D Lid Driven Cavity Analysis in Fluent 6.3
2D Flow over a plate Analysis in Fluent 6.3
Просмотров 4176 лет назад
2D Flow over a plate Analysis in Fluent 6.3
Airfoil NACA 0012 C-type Meshing in Gambit
Просмотров 3,9 тыс.6 лет назад
Airfoil NACA 0012 C-type Meshing in Gambit
Airfoil NACA 0012 O-type Meshing in Gambit
Просмотров 2 тыс.6 лет назад
Airfoil NACA 0012 O-type Meshing in Gambit
3D SuperSonic Nozzle Meshing in Gambit
Просмотров 3,1 тыс.6 лет назад
3D SuperSonic Nozzle Meshing in Gambit
2D SuperSonic Nozzle Meshing in Gambit
Просмотров 1,5 тыс.6 лет назад
2D SuperSonic Nozzle Meshing in Gambit
how to do dynamic meshing please suggest
In 9:58 the relevance center is removed in newer versions what should I do instead ?
J'ai un mémoire de fin d'études et le dessin sera en jeu. Pouvez-vous m'aider ?
i understand why u uploaded sad music..dude waited for 4 hours for the results xd
Bro change your system pls😅be khoda mn bodm rvani mishodam
can you tell why the minimum velocity is zero?
Hi sir, I took a picture from this video as a reference for my final project, I hope you will allow me to do what I did
Doing Cfd is depressing in itself and this music worsens it .
thank you sir for these videos ...but i want to know how to simulate spray strategy with fluent 6.3.26
oh god the music😂😂 BTW I really liked the video, thank you.
I get the error of negative cell. What can be the problem?
plz change this Song! it does not belong with this video
Why you did not use structured mesh for the nozzle?
how to generate the animation?
I have latest version 2020 2R ,some of tools are missing on my Version.it is better to upload a new vedio of rotating airfoil in 20202r
this doesn't work
how was the first step sir?
But why do these things i did not understand objective of all these
Good day. Thanks alot .I used this method to validate a journal (mixed convection in a lid driven cavity) by R iwatsu et al. The contours look alike but my nusselt number were off .. could you the vid for me or share me some tips thanks in advance
Whats with the music? CFD is enough to make me sad!
Thanks for the nice video tutorial. Do you have any tutorials of plasma actuator on airfoil or flat plate?
Did you find any tuturioal for this?
why gravitational acceleration in upward direction @15:40
Please can u help with a borehole heat exchanger please please 🙏🙏🙏😭😭😭😭
كيف افتح ملف gambit قمت بحفظه ؟
good evening Dr., do you have an active email ? it was very nice if we can discuss the CFD project at this time. here is my email : arifadtyasbudiman@yahoo.com
Sir please give the information about how did u imported the geometry..from we can get the geometry of airfoil
hey you can use airfoil tools(google it)
This can be done using the command import vertices data in the import list. The profile data should be saved as text file with first and last line of the data are (1,0,0) which corresponds to (x,y,z) for the trailing edge
dear sir How can I merge two symmetries in a single symmetry I get pressure and velocity only at the external zone rather than both
Hey! I kinda have a problem. It gives me an error saying there's a memory allocation failure. I've tried to run the calculations like thrice now and it gave me the same error every time. How do i get this to run the calculations? Any inputs would be appreciated !!!!!! Thanks.
Vishisht Adithyan this is the same issue I get when I was doing it for 777-9x airfoil with extragensis Yamaha R1
Modify the logarithmic decrement to e^-2.566 and change the sub coordinates to extrusion
Could u just share files. it will be helpful for the beginners.
I think files will help us
منم نجاتی ام
Good evening, how to make a vortex data turbin.txt ? Thanks
Sir,i need your help for my project.. Could you please help me how ro simulate a vapourisation of liquid... Please sir!
Coordinates pls
Hi, u can download it from here: drive.google.com/file/d/10KzPQuJegrVT9yERprIHm-tBp7dzxUV6/view?usp=sharing
thank u sir