Aerodynamics: CFD Meshing Tutorial of Airfoil with Deployed Flap / Slat (ANSYS Fluent & SolidWorks)

[@victordominguez4565]

I'm a prospectus applicant for an aerospace university with a bachelor's degree on aeronautics, I want to claim that you have done a really great job with your videos!! Simple, helpful, and nice explained! thanks for your knowledge! Best regards from Mexico!

[@joostin123]

Your orthogonal quality would be terrible with all your skewed elements, plus no inflation layer on the aerofoils as well

[@040_shivangpatni_aero3]

Your channel is a blessing

[@santoshmaharana4020]

gr8 effort on vd engineering and his weight:)

[@elguapo3436]

Are you serious about this mesh or more importantly about this procedure? Highly distorted elements in critical regions, with no boundary layer, how this is going to capture gradients. I've never seen the airfoil done this way.

[@saroj4736]

nice video ' do you have any video on dynamic meshing of airfoil i need to make a flapping airfoil

[@littlebitsunshine]

Great! Thank you very much!

[@shubhamkolhe2414]

Can you please make more videos on ansys fluent...

[@khalid26752]

Your videos are so great sir! Im doing some cfd for f1 wings, and Im facing some troubles I have a 3 elements wing, but I don't know how to calculate the planform area Should I adjust all the 3 elements to zero AoA, then taking the planform area? Or should I consider all the 3 elements as 1 indivisual wing and then taking the planform area? And if I did the second choice, should the equvalent wing be in zero AoA or what?? Please let me know

[@timothyoladapo8379]

Hey guys, does anyone how he created the planar surface for the aerofoil? As I get rebuild errors

[@ignamendi21]

can you make a video with a 3D airfoil wing with complex geometry? I am trying it and I dont know how to mesh it.....:(

[@tiklingmamatik4587]

hello sir good day, how to get the chord length of leading edge slat.?

[@aldossaryaldossary5209]

can i use qblade ?

[@Surya4331s]

Can you help me why enthalpy value is in negative in Ref. Value.

[@midhunashree7520]

thank u sir

[@lnr6110]

I want analysis of aerofoil (NACA0012) with gurney flap in CFD .Can u please make a video on it .

[@fouadzentout]

Did u find it?

[@aaronaloysius6320]

Hi theree im not getting the airfoil hole when i insert surface planar. Can u explain howw to fix that??

[@VDEngineering]

I don't do this anymore. Sorry

[@devanglabdhe60]

Did you get it ? I am facing the same issue.

[@vlaicuu]

Same issue

[@ultrasgrumese]

Hi guys, I'm creating a structured mesh in Icem with block, unfortunately I am having problems connecting the blocks between the fuselage, the horizontal and vertical tail plane, could someone help me? I am desperate, thank you

[@absarahmedkhan2109]

Is it not necessary to have a structured/face mesh for the slotted flaps? Will the results not come out inaccurate?

[@mohamedtarek3956]

Hey man, Great video first of all. I wanted to ask if you were familiar with morphing wings that are used in aircrafts. I was trying to do a moving mesh with the geometry changes. Do you have any idea what would be the ideal way to do it?

[@manelsouguir8126]

Sir , please can you tell me how had you removed blak lines in the text file ?

[@mohamedsalim7750]

U should have used Java foil to close the trailing edge points

[@mohamedsalim7750]

Over all it’s a great work from u, thank u

[@olooalfredo]

Vinayak How can I simulate flight at 30,000ft in Ansys fluent? I mean, how can I change the altitude... Zenkyu!

[@VDEngineering]

Change the pressure and density

[@olooalfredo]

@@VDEngineering okay. So which pressure is this. Outlet pressure (which is usually 0 gauge) or what? Or if only you could do a video on that...

[@ibrahimelkebsi783]

Hi everyone, I need help with my meshing of wing. I use inflation layers, but they aren´t continuous. And moreover, as you can see on the pic., some layers are bigger than rest. On the picture where are the layers continuous I use different wing without any twist, etc. Is here anyone, who can help please?

[@olooalfredo]

Where is the pic

[@rashidiqbal7282]

No used Ansys this work

[@aidealczar6075]

Hi, Just a question, whats the difference between splitting the face in solidworks or design modeler?

[@aidealczar6075]

Also why is the energy equation turned on?

[@riqyrizqyandra2206]

@@aidealczar6075 because your using ideal gas

[@mohammadaminabazari4298]

Could you shair design modeler or mesh files?

[@havafazai9023]

Ridi ba in English harf zadanet, oskol

[@archanakumari5876]

Leading edge radius how many %?

[@VDEngineering]

You can choose that, keep it realistic

[@archanakumari5876]

@@VDEngineering leading edge radius = to max chamber?

[@claudiafeurra5451]

Fluent version?

[@SomeTechGuy666]

Where can I get the geometry file for that air foil ?

[@VDEngineering]

The website

[@lorenzocarrattieri6952]

No that's a very bad mesh! Very distored in some regions and not properly defined to solve the boundary layer

[@VDEngineering]

It's been years. I don't do this anymore you told me too late lol

[@billhamilton2366]

Do you happen to have an e-mail address or facebook page where I can talk to you. I have a small airfoil project I need some help with. Thanks in advance. Bill Hamilton, Toronto.

[@olooalfredo]

Well,I can help

[@ultrasgrumese]

I can send you the icem file so you can see what's wrong if you want

[@Surya4331s]

send

[@akileshgokulakrishnan9658]

the tutorial is very fast and beginners can never follow them

[@VDEngineering]

Because it's not meant for beginners!!!

[@praweenthakur741]

Are you Indian