Multi-Airfoil Source/Vortex Panel Method

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  • Опубликовано: 20 авг 2024
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Комментарии • 10

  • @rickypalomares9786
    @rickypalomares9786 4 года назад +5

    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 года назад +3

      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.

  • @alexdoom7520
    @alexdoom7520 3 года назад +2

    .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.

  • @carlosmaldonado8600
    @carlosmaldonado8600 4 года назад +4

    Thanks Josh!

  • @migniondavis5942
    @migniondavis5942 3 года назад +1

    Yes, I did learn a lot and thank you so much!!!

    • @JoshTheEngineer
      @JoshTheEngineer  3 года назад

      Glad to hear it!

    • @migniondavis5942
      @migniondavis5942 3 года назад

      @@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 2 года назад

    Would this work in octave?