Aerospace Engineering > GATE 2023 > Aircraft Performance
An airplane with wing planform area of 20 m2 and weight 8 kN is flying straight and level with a speed of 100 m/s. The total drag coefficient is 0.026 and the air density is 0.7 kg/m3. The total thrust required to introduce a steady climb angle of 0.1 radians is _______ N. (round off to the nearest integer)

Correct : 1

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aerospace engineering GATE aerospace engineering 2023 airplane thrust calculation steady climb angle flight mechanics aerodynamics drag airplane performance calculation GATE 2023 Q59

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