A thin airfoil can be approximated as a flat plate. The airfoil
is set at an...
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Mechanical Engineering
A thin airfoil can be approximated as a flat plate. The airfoilis set at an angle of 10° to an air flow with Mach 2, a temperatureof –50°C, and a pressure of 50 kPa. Using linearized theory, findthe pressures on the upper and lower surfaces of this wing.
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Solutiongiven data 100 0174 radianM2 50 kPaUsing linearized
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