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1. |
Find liftoff distance for an aircraft which has weight of 20kN and thrust of 8kN. Consider thrust is much larger than drag and friction parameters. Consider maximum lift coefficient of 1.1, reference area of 12m2 and sea-level density. |
A. | 454m |
B. | 1000m |
C. | 12m |
D. | 12.12m |
Answer» B. 1000m | |