Air at -10C flows over a smooth, sharp-edged, almost-flat, aerodynamic surface at 240 km/hr. The surface...

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Air at -10°C flows over a smooth, sharp-edged, almost-flat, aerodynamic surface at 240 km/hr. The surface is at 10°C. Find (a) the approximate location of the laminar turbulent tran- sition; (b) the overall h for a 2 m chord; (c) h at the trailing edge for a 2 m chord; (d) 5 and h at the beginning of the transition region. [8x, should be around half a millimeter.] Air at -10°C flows over a smooth, sharp-edged, almost-flat, aerodynamic surface at 240 km/hr. The surface is at 10°C. Find (a) the approximate location of the laminar turbulent tran- sition; (b) the overall h for a 2 m chord; (c) h at the trailing edge for a 2 m chord; (d) 5 and h at the beginning of the transition region. [8x, should be around half a millimeter.]