Wind Turbine Aerodynamics - 5b - Unsteady Momentum Model

18 August 2026, Galih Bangga

Unsteady BEM

  1. unsteady inflow, unsteady excitation: $u, v, w = f(x, y, z, t)$
  2. apply corrections to standard BEM theory
  3. get correted output: $a, a' = f(x, y, z, t)$

Dynamic Wake

Approach to calculate the induced velocity on slide 11

Yaw Misalignment