Question: ) What is the maximum available thrust provided by the engine and propeller when it is operating at a flight altitude of 5,000ft? Give an

) What is the maximum available thrust provided by the engine and propeller when it is operating at a flight altitude of 5,000ft? Give an expression for the maximum available thrust as a function of the airspeed. Give an expression for the corresponding fuel flow rate as a function of airspeed.

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