The fuselage of a large transport aircraft has a diameter of 3.8 m and a length of 43 m. Determine the fuselage zero-lift drag, assuming the wing area to be 180 m2 and the cruising speed to be 350 knot at 35,000 ft.

The fuselage of a large transport aircraft has a diameter of 3.8 m and a length of 43 m. Determine the fuselage zero-lift drag, assuming the wing area to be 180 m2 and the cruising speed to be 350 knot at 35,000 ft.


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