If you increase your load factor by doing a high g turn, what happens to your aircraft's Specific Excess Power? (29.2)
A. |
It increases because the increased g s make the aircraft more maneuverable |
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B. |
It increases because the aircraft can turn better at high load factors |
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C. |
It decreases because more power is required to overcome the increased induced drag |
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D. |
It decreases because the aircraft is limited structurally to a maximum load factor. Since it is closer to this limit, it has less excess power. |
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