A helicopter is in hover, and it is found that the average velocity of the air right below the rotor is 30 m/s. If the r
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A helicopter is in hover, and it is found that the average velocity of the air right below the rotor is 30 m/s. If the r
A helicopter is in hover, and it is found that the average velocity of the air right below the rotor is 30 m/s. If the rotor diameter is 8 m, and the aircraft is operating at sea level (rho = 1.226 kg/m³), approximately how heavy is the helicopter? (in kg) (Use momentum theory to determine the answer)
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