Aerospace Engineering > GATE 2018 > Aircraft Performance
Gross weight of an airplane is 7000 N, wing area is 16 m2, and the maximum lift coefficient is 2.0. Assuming density at the altitude as 1.23 kg/m3, the stall speed (in m/s) of the aircraft is ________ (accurate to two decimal places).
Correct : 18.80 to 18.90
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