A thin flat plate is positioned in a wind tunnel parallel to the wind direction. A gas flows past this plate with a velocity of V = 2.0m/s . Assuming that the whole boundary layer is laminar, determine the kinematic viscosity of the gas if the boundary layer thickness is 19mm at a distance of x = 62cm along the plate. KinematicViscosity= m2/s . (Provide your answer to 6 decimal places)