From: Review of vortex methods for rotor aerodynamics and wake dynamics
Parameter | Value |
---|---|
Number of blades, NB [-] | 2 |
Chord length, c [m] | 0.1905 |
Rotor radius, R [m] | 1.143 |
Twist angle, θtwist [deg.] | 0 |
Blade planform | Rectangular blade |
Blade sectional profile | NACA 0012 airfoil |