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The main helicopter rotor of a conventional helicopter contains 4 blades and weighs 1 0 0 0 kg . The helicopter climbs at 7 .

The main helicopter rotor of a conventional helicopter contains 4 blades and weighs 1000 kg. The helicopter climbs at 7.2 m/s and the induced air speed in hover is 9.6 m/s. The main rotor speed is 252 rpm and the main rotor radius is 4,2 m. Calculate the total inflow ratio. Provide the numerical value only in the answer box, including any signs. Do not include any units in the answer box. Provide your answer to three decimal places.

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