Question: A propeller-driven aircraft with the characteristics given below has been designed to cruise for maximum range with zero elevator deflection. Determine the elevator deflection

A propeller-driven aircraft with the characteristics given below has been designed to cruise for maximum range with zero elevator deflection. Determine the elevator deflection required to cruise for maximum endurance. Characteristics: Zero-lift moment coefficient about c.g., CM.0 = 0.06 Lift-curve slope, a Parasite drag coefficient, CD, = 0.08 deg = 0.025 Drag polar parameter, K = 0.05373 Tail volume ratio, VH = 0.3 CLJ Elevator effectiveness, = 0.04 deg

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