Air at a temperature of 25°C flows over a smooth flat plate with a uniform velocity of 10 m/s along the plate. Find at what distance from the entrance of the plate will the boundary layer begin to transition to turbulence? For air at 25°C: p = 1.184 kg/m³ and μ = 1.849x10^-5 kg/(m·s).
0.854 m
1.261 m
0.156 m
0.074 m