Airfoil design with QBlade & Solidworks

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  • Опубликовано: 23 апр 2016
  • In this video we can see how to use Qblade and solidworks in order to design a custom wing with our custom airfoil
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Комментарии • 24

  • @cwrobinson6363
    @cwrobinson6363 8 лет назад

    Excellent! I like this video.

    • @MightyWings
      @MightyWings  8 лет назад

      +cwrobinson6363 thanks for watching

  • @medrasslen2894
    @medrasslen2894 3 года назад

    Thank you very much

  • @nicoclinco6028
    @nicoclinco6028 6 лет назад

    Grazie mille :D

  • @jonathanperezbernaldez8807
    @jonathanperezbernaldez8807 2 года назад

    Thanks a lot bro, it was very helful to activate it, everything except that in my flow simulation, when i must to select Dynamic pressure, it doesn't appear to me.. only "pressure", and the analysis doesnt appear to me the lift and drag forces.. What can i do?

  • @mflight569
    @mflight569 8 лет назад

    thanks bro.this video is very usefull

  • @fadoobaba
    @fadoobaba 8 лет назад

    very nice volume in this video.

    • @MightyWings
      @MightyWings  8 лет назад

      +fadoobaba thanks for watching. It took me a while mastering cubase...

  • @theminertom11551
    @theminertom11551 6 лет назад

    Hi, and thank you for the video. I do have one question however. When looking at the SolidWorks flow simulation I saw lots of high pressure on the top of the wing and low pressure towards the trailing edge of the wing. Is this not the reverse of what we would see if we had lift?

    • @MightyWings
      @MightyWings  6 лет назад

      What you see in flow simulation is dynamic pressure

    • @theminertom11551
      @theminertom11551 6 лет назад

      Thank you for the reply. I am not a propeller expert and I appreciate an opportunity to learn from you. My simple understanding was that due to Bernoulli's principle, the area of low pressure needed to be on top of the wing in order to create lift. Can you please explain what you mean by dynamic pressure?

    • @MightyWings
      @MightyWings  6 лет назад

      Lift force is directly proportional to dynamic pressure. If you look lift formula you will easy understand that

  • @111hemanth
    @111hemanth 7 лет назад

    can anybody post the download link for me as i cant download due to institutional limit in the download website

  • @DC.180
    @DC.180 8 лет назад

    Hi, thanks for the video, very helpful. I was wonder if you can upload a video for an kind of drag turbine design in Qblade and SW?
    Or do you know and quick-first-tet -steps guide?
    Thank you!

    • @MightyWings
      @MightyWings  8 лет назад

      +Daniel B. C. Cortés I'm preparing one, but i need more time...

  • @estaykylyshbek8347
    @estaykylyshbek8347 6 лет назад

    im doing an optimization for wind turbine blade based on camber line, which is the best option for 3d modelling

    • @MightyWings
      @MightyWings  6 лет назад

      If is only a study, qblade can give you the infomation you need.
      If you need to draw a blade, qblade has some limitations like parametric cad export file (solidworks, inventors etcc)

    • @medrasslen2894
      @medrasslen2894 3 года назад

      me too , do you have some advices?

  • @mohamednagi5317
    @mohamednagi5317 7 лет назад

    Hello There i want to ask about your PC specs as when i go to analyze part it tool to much time than you in the video and i want to know if it's a problem in my program or just PC specs difference
    i'm currently working on Core I3 with 6 GB of RAM

    • @MightyWings
      @MightyWings  7 лет назад +1

      +Mohamed Nagi hi, i'm using a 2010 intel i7 octacore with 24 gb xfury ddr3 1333 mhz

    • @mohamednagi5317
      @mohamednagi5317 7 лет назад

      Great sure it's all about specs, thanks a lot

  • @Gibbo263
    @Gibbo263 7 лет назад

    any way to put NACA number into theis, I cant get the illionos university and excel way to work

    • @MightyWings
      @MightyWings  7 лет назад

      +Gibbo263 yes of course, I made a video...I think is the second in my channel...
      However with illinois resource, you cannot made modifications on the geometry of the airfoil and the number of points is limited.
      Thanks for watching