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1. |
An aircraft is climbing with a 20° of climb angle and a 5° of angle of attack having a mass of 11,000 kg and aircraft thrust is 46082.75N then determine aircraft drag. |
A. | 33898.64 N |
B. | 52708.59 N |
C. | 82814.78 N |
D. | 8999.99 N |
Answer» E. | |