Multi-Airfoil Source/Vortex Panel Method

  Рет қаралды 5,186

JoshTheEngineer

JoshTheEngineer

Күн бұрын

Пікірлер: 12
@rickypalomares9786
@rickypalomares9786 4 жыл бұрын
This video series was fantastic. I have been following it since you started it and writing a few codes in parallel for fun, comparing to what I did in class awhile back. Thank you for making this.
@JoshTheEngineer
@JoshTheEngineer 4 жыл бұрын
Thanks for sticking around for the whole thing! It took a while to put it all together, but like you mention, it could be helpful to get a different perspective on the topic for others taking an aerodynamics course.
@realmrdoom
@realmrdoom 3 жыл бұрын
.Thank you so much for making these videos! I'm new to aerodynamics and these codes have helped me tremendously in understanding the source/vortex panel method.
@JoshTheEngineer
@JoshTheEngineer 3 жыл бұрын
You're welcome! Thanks for watching them!
@hu5116
@hu5116 2 ай бұрын
Josh this was fantastic! Thanks so much!
@frankovercrest2317
@frankovercrest2317 2 ай бұрын
How can we get the drag coefficient for two elements?
@migniondavis5942
@migniondavis5942 3 жыл бұрын
Yes, I did learn a lot and thank you so much!!!
@JoshTheEngineer
@JoshTheEngineer 3 жыл бұрын
Glad to hear it!
@migniondavis5942
@migniondavis5942 3 жыл бұрын
@@JoshTheEngineer I just want to thank you. As a result of your videos I was able to understand my aero course and complete the NACA project we received.
@jacewalton6677
@jacewalton6677 3 жыл бұрын
Would this work in octave?
@carlosmaldonado8600
@carlosmaldonado8600 4 жыл бұрын
Thanks Josh!
@JoshTheEngineer
@JoshTheEngineer 4 жыл бұрын
You're welcome!
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