Question: Air at -10C flows over a smooth, sharp-edged, almost-flat, aerodynamic surface at 240 km/hr. The surface is at 10C. Find (a) the approximate location
Air at -10C flows over a smooth, sharp-edged, almost-flat, aerodynamic surface at 240 km/hr. The surface is at 10C. 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.]
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To solve this problem we will use boundary layer theory for flow over a flat plate The Prandtl boundary layer equations and related formulas will help ... View full answer
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