Solution-Weightw 15000 lb wing area s 230 ft2 altitude

Weight(W) = 15000 lb, Wing area (s) = 230 ft^2, Altitude = sea level, temperature standard, AOA at stall = 20 degrees.

What is the airspeed associated with initial onset of stall? (KEAS)

If the gross weight is increased by 10%, how would the stall speed change?

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