Question
A)Calculate the clean stall speed (Vs) of the following aircraft (2 pts) Wing area: 174 sq ft CL max zero flaps: 1.22
A)Calculate the clean stall speed (Vs) of the following aircraft (2 pts)
Wing area: 174 sq ft
CL max zero flaps: 1.22
CL max full flaps: 1.7
Weight: 2,550 lbs
Standard density of 0.002377
Airfoil: modified NACA 2412 Standard day at Sea level conditions
B)Calculate the dirty stall speed (Vso) of the following aircraft (2 pts)
Wing area:174sqft
CL max zero flaps: 1.22
CL max full flaps: 1.7
Weight: 2,550 lbs
Standard density of 0.002377
Airfoil:modified NACA 2412 Standard day at Sea level conditions
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Understanding Business Statistics
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