Problem 1 Consider air at standard temperature and pressure flowing steadily over a smooth flat plate. The air flows with a free-stream velocity of 5 m/s and the plate has a length of 2 m. Calculate the boundary layer thickness 2 cm from the leading edge, and at the trailing edge of the plate at x

The flow rate of air through a through a pipe is 0.02 m5/s. a pitot static tube is placed in the flow. the radius of the pitot static tube is 1 mm. assuming the flow to be steady and the air to be at 300k, calculate the difference in total and static pressure if the diameter of the pipe is: (a) d 0.1 m d 0.05 m (c) d 0.01 m