The diameter of the propeller of an aircraft is 2.5 m. it flies at a speed...

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The diameter of the propeller of an aircraft is 2.5 m. it flies at a speed of 500 kmph at an altitude of 8000 m for flight to jet speed ratio = 0.75. determine i) The flow of air through the propeller, ii) Thrust produced, iii) Specific thrust, iv) Specific impulse, v) Thrust power. The diameter of the propeller of an aircraft is 2.5 m. it flies at a speed of 500 kmph at an altitude of 8000 m for flight to jet speed ratio = 0.75. determine i) The flow of air through the propeller, ii) Thrust produced, iii) Specific thrust, iv) Specific impulse, v) Thrust power.

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