Consider an airplane of wing area 31 m² (both wings combined) flying through air of density 1.18 kg/m³. From the plane's point of view, the air flowing above the plane's wings has speed 240 m/s, but the air flowing below the wings has speed 218 m/s. What is the net upward lift force on the plane? Assume laminar air flow both above and below the plane's wings. The plane is flying horizontally. 3

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Consider an airplane of wing area 31 m (both
wings combined) flying through air of density
1.18 kg/m³. From the plane's point of view,
the air flowing above the plane's wings has
speed 240 m/s, but the air flowing below the
wings has speed 218 m/s.
What is the net upward lift force on the
plane? Assume laminar air flow both above
and below the plane's wings. The plane is
flying horizontally.
3
Transcribed Image Text:2 Consider an airplane of wing area 31 m (both wings combined) flying through air of density 1.18 kg/m³. From the plane's point of view, the air flowing above the plane's wings has speed 240 m/s, but the air flowing below the wings has speed 218 m/s. What is the net upward lift force on the plane? Assume laminar air flow both above and below the plane's wings. The plane is flying horizontally. 3
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