Air at 100 kPa and 300 K blows over thin, smooth plate at 50 m/s. For this case we will assume boundary layer transitions to turbulent flow at Recrit = 500,000 and that velocity profile is provide by the power law function: u(y) U 1/7 = At both the plate midpoint (x = 0.5 m) and trailing edge (x = 1.0 m) compute: a) the boundary layer thickness (mm), b) the distance from the plate surface (y) where the velocity of the air is 1 m/s (mm), c) the velocity of the air 5 mm above the plate surface (m/s), d) the local shear stress (N/m). Compute the total drag force on the plate assuming boundary layer flow on both top and bottom surface considering that the boundary layer is partially laminar and partially turbulent. Air, 50 m/s 100 kPa, 300 K 1 m