No video

Panel methods [Aerodynamics #11]

  Рет қаралды 16,792

Prof. Van Buren

Prof. Van Buren

Күн бұрын

Lecture 11 is on Panel Methods, how we apply the elemental flow concepts to realistic aerodynamic shapes. It requires discretization of our body surface, and applying elemental flows to individual segments on the surface. Specifically, we look at the Source Panel Method and the Vortex Panel Method. By enforcing the "no penetration" boundary condition (normal velocity at the surface is zero), we can find the strength distributions of the sources or vortices to recreate the aerodynamic shape with streamlines.
Free downloadable notes (PDF with white background) can be found at my website: sites.udel.edu...

Пікірлер: 26
@fanBladeOne
@fanBladeOne 10 күн бұрын
The recaps at the end are a real strengthening tool.
@prof.vanburen
@prof.vanburen 2 күн бұрын
I think so too!
@radusewsk
@radusewsk 2 жыл бұрын
These classes are gold! Excellent work! Hope you keep it up, professor! Have a nice one! Cheers
@prof.vanburen
@prof.vanburen 2 жыл бұрын
Thanks and glad you like them!
@scarpredator5583
@scarpredator5583 Жыл бұрын
Can u tell me why I panel is surface instead of j panel???? The host didn't mention
@TheEngineeringHub
@TheEngineeringHub Жыл бұрын
Amazing video! Thank you Prof. Van Buren!
@prof.vanburen
@prof.vanburen Жыл бұрын
Glad you liked it!
@barbarahippauf413
@barbarahippauf413 7 ай бұрын
The explanations are perfect. Thanks for that❤
@prof.vanburen
@prof.vanburen 7 ай бұрын
Glad you liked it!
@tangleizhu5612
@tangleizhu5612 9 ай бұрын
Why is the correction at 13:28 is lambda/2 instead of any other numbers
@tangleizhu5612
@tangleizhu5612 9 ай бұрын
Thx in advance
@prof.vanburen
@prof.vanburen 8 ай бұрын
Hey thanks for your comment and sorry for getting to this so late! The semester got away from me. This lambda/2 is the mathematical solution for when i=j when solved out (in a complicated way that I certainly don't understand). So it isn't an arbitrary constant, but the true solution that accounts for our inability to do the solution simply due to dividing by zero. Hope this helps!
@9wyn
@9wyn 2 жыл бұрын
Are Panel Methods, Boundary Element Methods (BEM), and Boundary Integral Methods (BIM) different names for the same methods?
@prof.vanburen
@prof.vanburen 2 жыл бұрын
I had to recruit a math friend help because Boundary Element Methods are more general mathematics. As I understand it, Boundary Element Methods are ways to solve Boundary Integral Equations, where Boundary Integral Equations come from changing a PDE on some domain to an integral over that domain's boundary. Panel Methods are a specific subset of Boundary Element Methods applied to inviscid irrotational flow (which leads to the Laplace equation) with particular choices of boundary elements based on elementary flows.
@9wyn
@9wyn 2 жыл бұрын
Thank you prof Tyler van Buren.🙏🏽
@scarpredator5583
@scarpredator5583 Жыл бұрын
Can u tell me why I panel is surface instead of j panel???? The host didn't mention
@prof.vanburen
@prof.vanburen Жыл бұрын
Can you be a bit more specific? Generally, we look at the impact of a j-panel on an i-panel, and we end up adding all the surrounding j's. I'm not sure if this helps, but with more detail I might be a bit more helpful!
@sashaktakharel7365
@sashaktakharel7365 2 жыл бұрын
It would be great if you could do some numericals related to panel methods. having difficult time understanding them 😟😟😟
@prof.vanburen
@prof.vanburen 2 жыл бұрын
Something to think about moving forward! It's not my strength, so probably why I lean away from trying to dive deep into it. I share your struggles
@scarpredator5583
@scarpredator5583 Жыл бұрын
Can u tell me why I panel is surface instead of j panel???? The host didn't mention
@david_porthouse
@david_porthouse 2 жыл бұрын
Could we please see a suite of panel methods written in Excel VBA that anyone can download and run.
@prof.vanburen
@prof.vanburen 2 жыл бұрын
I'm all for open-source publicly available tools, I wish I was competent enough to make it happen!
@david_porthouse
@david_porthouse 2 жыл бұрын
@@prof.vanburen I could do it all but I just don't have the time. Apart from my day job, I am currently tackling Maxwell's equations. We could do with a two dimensional panel method being applied first of all to an aerofoil generated by a Joukowski transformation to build up confidence and to show how it's done, all in the public domain.
@lsrinivasan242
@lsrinivasan242 2 жыл бұрын
Can the white board be shared as a pdf?
@prof.vanburen
@prof.vanburen 2 жыл бұрын
Yep! The PDF versions of all the notes for both series can be found here: sites.udel.edu/vanburen/education/ Sometimes it helps to have the PDF to zoom in on small/messy handwriting.
@scarpredator5583
@scarpredator5583 Жыл бұрын
Can u tell me why I panel is surface instead of j panel???? The host didn't mention
Thin airfoil theory [Aerodynamics #12]
23:36
Prof. Van Buren
Рет қаралды 19 М.
Normal shock waves [Aerodynamics #18]
28:30
Prof. Van Buren
Рет қаралды 11 М.
Incredible Dog Rescues Kittens from Bus - Inspiring Story #shorts
00:18
Fabiosa Best Lifehacks
Рет қаралды 29 МЛН
Ik Heb Aardbeien Gemaakt Van Kip🍓🐔😋
00:41
Cool Tool SHORTS Netherlands
Рет қаралды 9 МЛН
Just Give me my Money!
00:18
GL Show Russian
Рет қаралды 643 М.
XFOIL and Panel Methods
17:05
the Science of Flight
Рет қаралды 10 М.
Lifting line theory [Aerodynamics #16]
22:15
Prof. Van Buren
Рет қаралды 21 М.
Building More Complex Potential Flows (Panel Methods)
10:30
JoshTheEngineer
Рет қаралды 5 М.
Airfoil Analysis . Vortex Panel Method . Development
16:45
AeroAcademy
Рет қаралды 10 М.
Kutta Joukowski theorem [Aerodynamics #10]
16:00
Prof. Van Buren
Рет қаралды 35 М.
Source Panel Method: Normal Velocity Geometric Integral [I(ij)]
21:58
JoshTheEngineer
Рет қаралды 7 М.
The Most Mind-Blowing Aspect of Circular Motion
18:35
All Things Physics
Рет қаралды 695 М.
Vortex Lattice Method
30:16
BYU FLOW Lab
Рет қаралды 7 М.
Incredible Dog Rescues Kittens from Bus - Inspiring Story #shorts
00:18
Fabiosa Best Lifehacks
Рет қаралды 29 МЛН