Wind Tunnel - Pressure (Assignment) : Wind energy Labs : Mechanical Engineering : Amrita Vishwa Vidyapeetham Virtual Lab

Wind Tunnel - Pressure

	Wind Tunnel Fundamentals Theory Procedure Self Evaluation RT Assignment Reference Feedback Data Set

Integrate the pressure distribution over the airfoil to obtain the Lift and Drag forces. (See Anderson)
Plot the coefficient of pressure vs x/c along the airfoil chord.
From the resultant aerodynamic forces, obtain the torque and power of the turbine. (3 NACA 2415 blades)

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