For a given airplane with a given wing loading executing a turn in the vertical plane, under what conditions will the turn radius be minimum and the turn rate be maximum?
(A) Highest possible $C_{L}$ and lowest possible load factor
(B) Lowest possible $C_{L}$ and lowest possible load factor
(C) Lowest possible $\mathrm{C}_{\mathrm{L}}$ and highest possible load factor
(D) Highest possible $\mathrm{C}_{\mathrm{L}}$ and highest possible load factor

Question ID - 155930 :-

For a given airplane with a given wing loading executing a turn in the vertical plane, under what conditions will the turn radius be minimum and the turn rate be maximum?
(A) Highest possible $C_{L}$ and lowest possible load factor
(B) Lowest possible $C_{L}$ and lowest possible load factor
(C) Lowest possible $\mathrm{C}_{\mathrm{L}}$ and highest possible load factor
(D) Highest possible $\mathrm{C}_{\mathrm{L}}$ and highest possible load factor

1 Answer

5876 Votes

3537

Answer Key : (D) -

(D) Highest possible $\mathrm{C}_{\mathrm{L}}$ and highest possible load factor

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