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The diameter of the propeller of an aircraft is 2.5m; It flies at a speed of 500 kmph at an altitude of 8000m. For

The diameter of the propeller of an aircraft is 2.5m; It flies at a speed of 500 kmph at an altitude of 8000m. For a flight to jet speed ratio of 0.75 determine (a) the flow rate of air through the propeller, (b) thrust produced, (c) Specific thrust, (d) specific impulse and (e) the thrust power.

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