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Compute stall speed in knots equivalent airspeed (KEAS) for aircraft with the following conditions: Weight = 10,000 lbs Altitude = Sea level Wing area =100

Compute stall speed in knots equivalent airspeed (KEAS) for aircraft with the following conditions:

Weight = 10,000 lbs

Altitude = Sea level

Wing area =100 ft2

CL =1.6

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