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...

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 O^OC. The density of the air is 1.3 kg/m³
and viscosity is .023 CP at this temperature.