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 engine thrust.

A. 5257.79 N
B. 1810.97 N
C. 28013.99 N
D. 46082.75 N
Answer» E.


Discussion

No Comment Found