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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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