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RANS Simulations of Aerodynamic Performance of NACA 0015 Flapped Airfoil
- Sohaib Obeid,
- Ratneshwar Jha and
- Goodarz Ahmadi
An analysis of 2D subsonic flow over an NACA 0015 airfoil with a 30% trailing edge flap at a constant Reynolds number of 106 for various incidence angles and a range of flap deflections is presented. The steady-state governing equations of continuity...

