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The document summarizes an experiment to measure lift and drag coefficients of an airfoil as functions of angle of attack and Reynolds number using a wind tunnel. Key steps include: 1) calibrating wind speed in the tunnel; 2) measuring pressures on the airfoil surface using pressure transducers; 3) calculating lift and drag forces by integrating pressures; and 4) determining lift and drag coefficients while varying angle of attack and Reynolds number. The experiment uses a NACA 2415 airfoil model, wind tunn

Author

zeeshan khan

Language

EN