Aerospace Engineering > GATE 2016 > Aircraft Performance
A glider weighing 3300 N is flying at 1000 m above sea level. The wing area is 14.1 m2 and the air density is 1.23 kg/m3 Under zero wind conditions, the velocity for maximum range is _______ m/s.

Correct : 20.0: 21.0

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Related Topics

glider maximum range maximum range velocity aerospace engineering GATE 2016 GATE AE 2016 Q53 glider flight performance flight mechanics aircraft performance zero wind conditions

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