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If so instructed by your teacher, print out a worksheet page for these problems. |
Open FoilSim and set initial conditions as follows:
Airspeed (velocity) = 50 km./hr.
Altitude = 5000 m.
Angle = 1 deg.
Thickness = 12.5
Camber = 12.5
Area = 5 sq. m.
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- What is the lift in Newtons required to maintain altitude in these conditions?
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- What is the velocity that is required to maintain this lift?
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- What is the lift in Newtons now required to maintain altitude?
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- What is the velocity that is now required to generate the lift?
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