Estimate the drag force on an airplane wing

Reference no: EM131514972

Question: In order to estimate the drag force on an airplane wing, model the wing as a half-cylinder for the leading edge and as two flat plates for the upper and lower surfaces. Estimate the drag force for a wing approximately 15 cm thick, 10 m long and 2 m wide on an airplane traveling at 100 m/s in air at 0°C. The density of the air is 1.3 kg/m3 and viscosity is .023 CP at this temperature.

Reference no: EM131514972

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