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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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