Boundary Layer Characteristics
- The velocity gradients
within the boundary
layer and wake regions
are much larger than
those in the remainder
of the flow fluid
- Therefore, viscous
effects are confined to
the boundary layer and
wake regions
Transition occurs at
\[
\mathrm{Re}_{xcr}=\frac{\rho U x}{\mu}=2\times10^{5}\ \sim\ 3\times10^{6}
\]
depending on surface roughness and amount of turbulence in upstream flow
Distortion of a fluid particle as it flows within the boundary layer
Typical characteristics of boundary layer thickness and wall
shear stress for laminar and turbulent boundary layers
The Navier-Stokes equations are too complicated that
no analytical solution is available. However, for large
Re, simplified boundary layer equations can be
derived.
- The boundary layer assumption is based on the fact
that the boundary layer is thin
- Physically, the flow is parallel to the plate and any fluid is
convected downstream much more quickly than it is diffused
across the streamlines
- For boundary layer flow over a flat plate the pressure is
constant. The flow represents a balance between viscous
and inertial effects, with pressure playing no role
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