airplan crusing at sea level (density 1.225 kg/m3) the gross weight of the airplan is 500ON, the wing Span and theaspect ratio are 8 and 6 respectively. If the lift coeffeicent is 1.2 determine the speed of the airplan in m/s?

airplan crusing at sea level (density 1.225 kg/m3) the gross weight of the airplan is 500ON, the wing Span and theaspect ratio are 8 and 6 respectively. If the lift coeffeicent is 1.2 determine the speed of the airplan in m/s?

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Question

airplan crusing at sea level (density
1.225 kg/m3) the gross weight of the
airplan is 500ON, the wing Span and
theaspect ratio are 8 and6
respectively. If the lift coeffeicent is 1.2
determine the speed of the airplan in
m/s?

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