Find a the approximate location of the laminar turbulent

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Reference no: EM13645348

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

Reference no: EM13645348

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