Correction
Aeropropulsive Performance Modelling of Over-The-Wing Propulsion at Incidence (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023)
H.N.J. Dekker (TU Delft - Wind Energy)
Marthijn Tuinstra (Royal Netherlands Aerospace Centre)
W.J. Baars (TU Delft - Aerodynamics)
F. Scarano (TU Delft - Aerodynamics)
D. Ragni (TU Delft - Wind Energy)
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Abstract
Equation 3 for the induced velocity factor a in the section III.B should be: (Formula presented) Instead of: (Formula presented) The first sentence of Chapter V should read that an angle of attack of 8° positions the propeller in a strong adverse pressure gradient, not a strong advance ratio.