The four-seat light airplane Piper PA-34 has a horizontal tail with the following features: The aircraft has a mass of 2154 kg, a wing area of 19.39 m2, and is cruising at 171 knot at an altitude of 18,500 ft. Determine the horizontal tail zero-lift drag coef‑cient.

The four-seat light airplane Piper PA-34 has a horizontal tail with the following features:

The aircraft has a mass of 2154 kg, a wing area of 19.39 m2, and is cruising at 171 knot at an altitude of 18,500 ft. Determine the horizontal tail zero-lift drag coef‑cient.


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