Find the regime of the boundary layer at the location of (0.1 mathrm{~m}) from the leading edge
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Find the regime of the boundary layer at the location of \(0.1 \mathrm{~m}\) from the leading edge of an aerofoil, if the airspeed is \(80 \mathrm{~ms}^{-1}\), and air condition is at that of sea level. What is the regime if the aircraft travels at the same airspeed at \(10,000 \mathrm{ft}\) ?
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