Aerodynamics: CFD Meshing Tutorial of Airfoil with Deployed Flap / Slat (ANSYS Fluent & SolidWorks)
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- Опубликовано: 27 апр 2019
- #Ansys #Aerodynamics #CFD #Fluent #Airfoil
RESOURCES:
Airfoils: mail.tku.edu.tw/095980/airfoil...
VIDEO TIMESTAMPS:
Airfoil Basics (Parameters): 00:19
NACA Airfoil: 01:15
Importing Airfoil Geometry into SolidWorks: 01:32
Adding Flaps and Slats: 03:50
Structured (Face) 2D Meshing: 06:20
Hey Everyone
This video dives into the topic of Computational Fluid Dynamics (CFD). I will teach you how to perform structured (face) CFD meshing and simulation of an aircraft wing airfoil, with deployed flap s and slats. These simulations are typically performed to evaluate an aircraft wing's performance during takeoff and landing, as flaps / slats are deployed. These control surfaces increase the amount of lift (and corresponding drag) that the wing produces.
We will use SolidWorks as the primary CAD software, however other CAD packages such as CATIA, NX and Autodesk can also be used. The simulation will be performed in ANSYS Fluent.
The topics covered in this video include
1) Airfoil Geometry
2) Solidworks sketching and surface creation
3) ANSYS: Face Splitting, Face Meshing, Importing Geometry, CFD, Turbulence, Meshing, Mesh Sizing
Hope you learn something new! Be sure to subscribe to my channel for more Aerospace Engineering simulations and other content!
Relevant Videos:
CFD Structured Meshing: • ANSYS CFD Meshing Basi...
Rocket Nozzle CFD: • ANSYS Fluent: Rocket E...
Best Wishes,
Vinayak D.
VDEngineering
~~My Udemy Courses on Motion Planning / Navigation / Trajectory Planning:
www.udemy.com/course/autonomo...
My Instagram: / vinayak_desh
My Website: www.vinayakd.com/
Your channel is a blessing
gr8 effort on vd engineering and his weight:)
Your orthogonal quality would be terrible with all your skewed elements, plus no inflation layer on the aerofoils as well
Great! Thank you very much!
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!
thank u sir
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?
nice video '
do you have any video on dynamic meshing of airfoil i need to make a flapping airfoil
Sir , please can you tell me how had you removed blak lines in the text file ?
Is it not necessary to have a structured/face mesh for the slotted flaps? Will the results not come out inaccurate?
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
hello sir good day, how to get the chord length of leading edge slat.?
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
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.....:(
Can you help me why enthalpy value is in negative in Ref. Value.
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?
Where is the pic
Can you please make more videos on ansys fluent...
Hey guys, does anyone how he created the planar surface for the aerofoil? As I get rebuild errors
can i use qblade ?
Where can I get the geometry file for that air foil ?
The website
Hi, Just a question, whats the difference between splitting the face in solidworks or design modeler?
Also why is the energy equation turned on?
@@aidealczar6075 because your using ideal gas
I want analysis of aerofoil (NACA0012) with gurney flap in CFD .Can u please make a video on it .
Did u find it?
Fluent version?
Could you shair design modeler or mesh files?
Ridi ba in English harf zadanet, oskol
Vinayak How can I simulate flight at 30,000ft in Ansys fluent? I mean, how can I change the altitude...
Zenkyu!
Change the pressure and density
@@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...
Hi theree im not getting the airfoil hole when i insert surface planar. Can u explain howw to fix that??
I don't do this anymore. Sorry
Did you get it ? I am facing the same issue.
Same issue
U should have used Java foil to close the trailing edge points
Over all it’s a great work from u, thank u
Leading edge radius how many %?
You can choose that, keep it realistic
@@VDEngineering leading edge radius = to max chamber?
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.
Well,I can help
I can send you the icem file so you can see what's wrong if you want
send
the tutorial is very fast and beginners can never follow them
Because it's not meant for beginners!!!
No that's a very bad mesh! Very distored in some regions and not properly defined to solve the boundary layer
It's been years. I don't do this anymore you told me too late lol
Are you Indian