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  1. mezah

    Wing and blade aerodynaimc center

    i reversed the twist angles from root to tip instead from tip to root and it looks like this But it still different from the original one and i don't have another reference to compare with
  2. mezah

    Wing and blade aerodynaimc center

    As you can see in the figure below there is a point point where the lift and drag act and the angle is measured ( specially twist angle) it is mentioned before - in the book 'wind energy explained' - that the point is c/4 Taking in consideration that it is only one section and we must have N...
  3. mezah

    Wing and blade aerodynaimc center

    Hello everyone, Now i am trying to model wind turbine blade using solidworks. I have the airfoil coordinates at each section of the blade, but the coordinates are distance per chord (x/c,y/c) so i have to scale it using the calculated chord. When i scale it with respect to the origin - which is...
  4. mezah

    Question aboutTrefftz plane analysis?

    Unfortunately, there is no solved example for this course
  5. mezah

    Question aboutTrefftz plane analysis?

    KENAT i agree with you, incompressible flow is a safe assumption when we are dealing with HAWT since the speed and hence the Mach number are small. rb1957 This method used - as i understand - to calculate the induced drag, and since the induced is caused by the downwash which lead to change the...
  6. mezah

    Question aboutTrefftz plane analysis?

    All my respect to the rules but i am not searching for someone to solve my home work - that if i have one - all i need is a text book or a paper where i can find more detailed discussion about the subject rather than just a part of a presentation which is a little bit obscure for me. I asked...
  7. mezah

    Question aboutTrefftz plane analysis?

    Thanks for the link but i was hoping for some kind case study or at least solved examples
  8. mezah

    Question aboutTrefftz plane analysis?

    Hello every one I would like to learn more about trefftz plane theory which is used to calculate induced drag. Is it an effective method to calculate induced drag? can i used it with propeller and wind turbine instead of an aircraft wing? thanks in advance
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