Suppose a low-speed aircraft is flying at an altitude of 3000 m at an altitude of 360
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Suppose a low-speed aircraft is flying at an altitude of 3000 m at an altitude of 360 km/h. If the wing area is 40 m2, the average chord length is 2.5 m. Try to estimate the frictional resistance of the wing (calculated by complete turbulence) using the calculation formula of the two-dimensional flat plate boundary layer.
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