1.

A prop driven aircraft has propeller efficiency of 0.92 and C as 0.000745 1/m. If lift to drag ratio is 14 and weight fraction as 1.145 then, find range of the propeller driven aircraft.

A. 2340.95m
B. 2340.5miles
C. 2340km
D. 2500miles
Answer» B. 2340.5miles


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