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Define aerofoil with accepted terminology with neat sketch. A kite which may be assumed to be a flat plate and mass 1 kg soars at an angle to the horizontal. The tension in the string holding the kite is 60N when the wind velocity is 50 km/hr horizontally and angle of string to the horizontal direction is `35^0`. The density of air is 1.2 kg/`m^3`. Calculate the drag coefficient for the kite in the given position if the lift coefficient in the same position is 0.45. Both coefficients have been used in the full area of the kite. [ 2068-Shrawan ] [8]

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