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Which of the following is correct?(a) Elevator can float in stick free condition(b) Drag is always same as weight(c) Power loading is same as weight(d) Stability is same for every aircraftI got this question in examination.This intriguing question comes from Stick-Free Stability in division Stability, Control, and Handling Qualities of Aircraft Design

Answer»

The CORRECT answer is (a) ELEVATOR can float in stick free condition

Explanation: Stick free condition allows floating of elevator. POWER loading is defined as the ratio of weight of the AIRCRAFT to the power produced. Stability of aircraft DEPENDS on the design requirements. Military aircraft is less stable whereas commercial are more stable.



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