Airfoil analysis with Xfoil

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  • Опубликовано: 20 авг 2024
  • Analysis was done for Project 2 in EAS3101

Комментарии • 12

  • @ammarshafique9064
    @ammarshafique9064 4 дня назад

    Very very impressive!

  • @lucacasaletto8748
    @lucacasaletto8748 3 месяца назад

    used this tutorial to help validate my CFD results for uni, flaps part was especially helpful as i had no other way to validate them! Many thanks!

  • @Ale-kc9pq
    @Ale-kc9pq 2 месяца назад

    Thank you

  • @Cryptic_Chai
    @Cryptic_Chai Год назад +3

    Is there a non manual way to change the text file format? Like a C code or something.

  • @AngusMcAlister14
    @AngusMcAlister14 Год назад

    very nice video, thank you

  • @franciscopastormarti7009
    @franciscopastormarti7009 2 года назад

    yo´re the best, thnak U very much

  • @Aditya_yd27
    @Aditya_yd27 2 года назад

    Thank you 🙏

  • @andrescano2700
    @andrescano2700 Год назад

    What is the CDp column?

    • @elarabibabas6928
      @elarabibabas6928 Год назад

      drag coefficient , consists of 2 components: the cdf , due to friction and viscous phenomena and cdp (the one you are referring to) , which is the drag caused by the shape of the airfoil (it exists and in non viscous flows)

  • @kushaldgowda9519
    @kushaldgowda9519 2 года назад

    How to export cp graph to excel file from xfoil?

    • @spaceshuttle8332
      @spaceshuttle8332 Год назад

      There's a command in XFOIL called CPWR with allows you to write your x vs Cp values to a file

    • @kushaldgowda9519
      @kushaldgowda9519 Год назад

      @@spaceshuttle8332 Working. Thanks ya