Required information Air at 25°C and 1 atm is flowing over a long flat plate with a velocity of 6 m/s. The density and kinematic viscosity of air at 1 atm and 25°C are p = 1.184 kg/m3 and v= 1.562x10-5 m2/s. Determine the thickness of the boundary layer at the location of the plate where the flow becomes turbulent The thickness of the boundary layer is cm.
Required information Alr at 25°C and 1 atm is flowing over a long flat plate with a velocity of 6 m/s. The density and kinematic viscosity of air at 1 atm and 25°C are p=1184 kg/m3 and v=1.562x10-5 m2/s. Calculate the distance from the leading edge of the plate where the flow becomes turbulent. The distance from the leading edge of the plate is 1.30167 m.