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 drag is 9,000 N then determine aircraft lift.

A. 11453.17 N
B. 9220.07 N
C. 11553.17 N
D. 97385.85 N
Answer» C. 11553.17 N


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