An experimental study on aerodynamics of NACA2415 aerofoil at low Re numbers

@article{Gen2012AnES,
  title={An experimental study on aerodynamics of NACA2415 aerofoil at low Re numbers},
  author={M. Genç and Ilyas Karasu and H. H. Açikel},
  journal={Experimental Thermal and Fluid Science},
  year={2012},
  volume={39},
  pages={252-264}
}
Abstract This study is a detailed experimental investigation on aerodynamics of a NACA2415 aerofoil by varying angle of attack from −12° to 20° at low Reynolds number flight regimes (0.5 × 10 5 to 3 × 10 5 ). For this investigation, pressure distributions over the aerofoil were measured using a system including a pitot-static tube, a scanivalve unit and a pressure transducer. Moreover, time-dependant lift and drag forces and pitch moment of the aerofoil were obtained by using an external three… Expand
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