A single-engine small aircraft has a wing area of 26 m2 and a turboprop engine that has a power of 600 hp. The aircraft is cruising at 25,000 ft altitude at a speed of 182 knot. Determine the engine cooling drag coef‑cient. The air temperature at the exit is 400 K; and assume Ke = 2.

A single-engine small aircraft has a wing area of 26 m2 and a turboprop engine that has a power of 600 hp. The aircraft is cruising at 25,000 ft altitude at a speed of 182 knot. Determine the engine cooling drag coef‑cient.

The air temperature at the exit is 400 K; and assume Ke = 2.


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