Chapter 1 : Boundary Layer INTRODUCTION The condition of zero fluid velocity at the solid surface is referred to as ‘no slip’ and the layer of fluid between the surface and the free stream fluid is termed BOUNDARY LAYER. 1 Chapter 1 : Boundary Layer 2 Chapter 1 : Boundary Layer Shear stress, τ ∂u τ =µ ∂y Reynolds number The criterion which determines whether flow is laminar or turbulent. Reynolds number along a smooth flat plate: ρU s x U s x Re x = = µ υ Re < 5 x 105 : Laminar Re ≈ 5 x 105 : Transition (Engineering critical Reynolds number) Re > 5 x 105 : Turbulent 3 Chapter 1 : Boundary Layer 4 Chapter 1 : Boundary Layer Turbulent layer usually has a greater velocity gradient at the surface, which cause greater shear stress. From a turbulent layer, there is a more ready interchange of particles with the main flow, and this explains the more rapid increase in thickness of a turbulent layer. The thickness of a laminar boundary layer increases as x0.5 (when pressure is uniform), a turbulent layer thickens approximately as x0.8. 5 Chapter 1 : Boundary Layer BOUNDARY LAYER IN PIPE Laminar flow; Re < 2000 120 pipe diameters (=120D) Turbulent flow; Re > 2000 60 pipe diameters (=60D) 6 Chapter 1 : Boundary Layer DEFINITION z Boundary layer thickness, δ z Displacement thickness, δ* z Momentum thickness, θ BOUNDARY LAYER THICKNESS, δ Boundary layer thickness is defined as that distance from the surface where the local velocity equals 99% of the free stream velocity. δ = y(u =0.99U ) s 7 Chapter 1 : Boundary Layer DISPLACEMENT THICKNESS, δ* The displacement thickness for the boundary layer is defined as the distance the surface would have to move in the y-direction to reduce the flow passing by a volume equivalent to the real effect of the boundary layer. δ =∫ * δ 0 u (1 − )dy Us 8 Chapter 1 : Boundary Layer MOMENTUM THICKNESS θ Momentum thickness is the distance that, when multiplied by the square of the free stream velocity, equals the integral of the momentum defect. Alternatively, the total loss of momentum flux is equivalent to the removal of momentum through a distance θ. It is a theoretical length scale to quantify the effects of fluid viscosity near a physical boundary. δ θ =∫ 0 u ⎛ u ⎞ ⎜⎜1 − ⎟⎟dy Us ⎝ Us ⎠ 9