SHIJU R S
ASSISTANT PROFESSOR
DEPARTMENT OF MECHANICAL ENGINEERIN
GOVERNMENT ENGINEERING COLLEGE BARTO
THIRUVANANTHAPURAM
, Boundary Layer
The concept of boundary layer was first introduced by L. Prandtl in 1904.
“When a real fluid of low viscosity flows over a solid surface, developing a narr
fluid region close to the solid surface, having large velocity gradients and shear
stresses. This narrow region of fluid close to the boundary surface of the solid i
known as Boundary layer’’(Friction layer).
, Boundary Layer
Growth of boundary layer over a flat plate
Consider the flow of fluid having free stream velocity (U) over a smooth flat pla
which is placed parallel to the direction of flow as shown in figure
, Boundary Layer
Growth of boundary layer over a flat plate
The edge of plate facing the direction of flow is called leading edge and the rear
is called the tailing edge.
Near the leading edge, the boundary layer is wholly laminar. Where the velocity
distribution is parabolic.
The thickness of the boundary layer (δ) increases with distance from the leading
x, becomes unstable and breaks into turbulent boundary layer over a transition re
For a turbulent boundary layer, if the boundary is smooth, the roughness projecti
are covered by a very thin layer which remains laminar, called laminar sublayer