- Number of engines: 2 - Wing surface: S =

- 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
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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2. 21 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
3. 545 views
Number of engines: 2Wing surface: s=88.3 m^2 Diameter of engine inlet: d=1.1180 m Oswald efficiency: e=0.67 Span: b= 23.7m Mass:
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2. asked by shawon
3. 72 views
Number of engines: 2Wing surface: 88.3m Diameter of engine inlet: 1.1180 Oswald efficiency: 0.67 Span: 23.7 Mass: 30000 (ISA)
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2. 11 views
Find the pressure difference on an airplane wing where air flows over the upper surface with a speed of 119 m/s, and along the
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2. asked by Kim
3. 720 views
On a particular airplane wing, air flows over the upper surface with a speed of 115 m/s and along the bottom surface with a
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2. asked by Francisco
3. 606 views
Which of the following 'solutions' could reduce the drag of an aircraft? (Multiple answers can be correct)Reduce the wing
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2. 28 views
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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2. 24 views
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
1. 1 answer
2. 21 views