Wind Turbine Aerodynamics - Lecture

18 July 2026, Pascal Weihing

Balde design requirements

From blade root to blade tip:

Further requirements (not aerodynamic)

Airfoils in the inner blade region are dominated by structural properties - high rel. thickness, drag is aerodynamically less important than lift
Flatback airfoils can reduce the risk of flow separation: At the base of the trailing edge a negative pressure remains, less adverse pressure gradient needed from the point of maximum thickness to the trailing edge. The remaining negative pressure at the trailing edge is recovered in the airfoils wake

Reynodls number increases in the inner to mid blade region:

Reynolds number reaches maximum in the mid blade region because of having a large chord and high velocity

Reynolds number decreases to about 3 to 5 m at the outer blade region