Number of engines: 2 Wing

Number of engines: 2Wing area (S): 88.3 m² Diameter (d): 1.1180 m Oswald efficiency factor (e): 0.67 Wing span (b): 23.7 m
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Mass 500,000 kgWing Area 845 m2 Wingspan 79.75 m Number of Engines 4 CLmax flaps retracted 1.9 CLmax flaps extended 2.6 Oswald
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Mass 500,000 kgWing Area 845 m2 Wingspan 79.75 m Number of Engines 4 CLmax flaps retracted 1.9 CLmax flaps extended 2.6 Oswald
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Wing Area 845 m2Wingspan 79.75 m Number of Engines 4 CLmax flaps retracted 1.9 CLmax flaps extended 2.6 Oswald Efficiency Factor
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Variable ValueMass 250.000 kg Wing Area 511 m2 Wingspan 60.0 m Number of Engines 4 Distance from aerodynamic center of wing-body
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Mass 250.000 kgWing Area 511 m2 Wingspan 60.0 m Number of Engines 4 Distance from aerodynamic center of wing-body to the tails
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Mass 250.000 kgWing Area 511 m2 Wingspan 60.0 m Number of Engines 4 Distance from aerodynamic center of wing-body to the tails
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2. 15 views
Mass 250.000 kgWing Area 511 m2 Wingspan 60.0 m Number of Engines 4 Distance from aerodynamic center of wing-body to the tails
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2. 15 views
an aeroplane has a mass of 15 tonnes. At cruising speed,air flows over the top of it's wing at 150 m/s and under the wing at
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2. asked by Kay
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- Number of engines: 2- Wing surface: S = 88.3 m2 - Diameter of engine inlet: d = 1.1176 m - Oswald efficiency: e = 0.67 - Span:
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2. 15 views