Blade Element Momentum (BEM) for propellers and turbines: part 1 linear and angular momentum

แชร์
ฝัง
  • เผยแพร่เมื่อ 10 ธ.ค. 2024

ความคิดเห็น • 8

  • @dormg22
    @dormg22 2 ปีที่แล้ว +2

    amazing channel, thank you so much for uploading these lessons professor

  • @apocalypt0723
    @apocalypt0723 2 ปีที่แล้ว +3

    Thank you so much for the lectures. Learning so much from them

  • @TwanElshof
    @TwanElshof 25 วันที่ผ่านมา

    How do we get from T=2a(1+a)
    ho\V_inf^2A_d to T ' = 4a(1+a)
    ho\V_inf^2 pi r

  • @casper6349
    @casper6349 2 ปีที่แล้ว

    At 35:56, you are missing a V_\infty in the equation for torque. Furthermore, in case you would insert the velocity to arrive at the same equation as 34:08, you would end up at torque in terms of units, not torque per unit length. Won't this mess up the integration over the span later on in the calculations?

    • @BYUFLOWLab
      @BYUFLOWLab  2 ปีที่แล้ว +1

      Good catch, I indeed made a typo on the slide and the V_\infty should be there. With the Vinf include you do get the correct units (torque per unit length, N*m/m or just N). Fortunately, when I combine the momentum and blade element parts in the next video I have the V_\infty term back in so everything else is correct - just a typo on that slide.

  • @samdougherty5559
    @samdougherty5559 ปีที่แล้ว

    So from my understanding, for most of the calculations in this video the units are in Torque and Thurst. It is only when you make A_d = 2*pi*r*(dr) and then divide LHS and RHS by (dr) do the equations become Torque per unit length and Thrust per unit length?

  • @grahamflowers
    @grahamflowers ปีที่แล้ว

    There is something wrong with Betz limit if kinetic energy in the wind is 1/2 mass or 50% and Betz limit is 0.5926% then where can the 0.926% come from not the wind ? regards Graham Flowers MEng