Airfoil specifications

Airfoil Type

NACA0018

Chord length: c

110 mm

Flap height: h

0 mm, 4 mm, 6 mm

Flow and airfoil setting conditions

Inlet velocity: V

12 m/s

Reynolds number

8.8 × 10⁴

h/c

0.0, 0.036, 0.055

Range of angle of attack (AOA)

−5˚ - 10˚