3 3 calculate lift and drag forces and coefficients 1 consider an airc
Calculate lift and drag forces and coefficients
1. Consider an aircraft wing the has an area of 500m. The aircraft
is travelling at 200m/s through air that has a density of 0.8
kgm. The lift coefficient of the wing is 0.65. Calculate the lift
force generated under these circumstances.
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2. A model wing is placed in a wind tunnel. The velocity of air in
the tunnel is 50m/s with a density of 1.2kqm. The drag force
generated is 6kN over an area of 7m. Calculate the drag
coefficient of the wing.
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