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This is the second course of a two-semester fluid mechanics sequence for graduate students in the thermal sciences. This course includes topics like fully turbulent flows, turbulent boundary layers and free shear flows, turbulence modeling, laminar boundary layers including axisymmetric and 3-D boundary layers. Key points in this lecture are: 3-D Boundary Layer Cone, Scale Factors, Geometry, Scale Factors or Stretching Factors, 3-D Coordinate System, Axisymmetric Boundary Layers, Boundary Layer
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Y
r
y
α
x
α
R α
G
r 0
P
Z
z or θ
n
G
X
X - Z plane
z or θ
r 0
θ
y
P
Y
X
r
X
Y
3-D view, in x-y plane ( X-Z plane is tilted back as shown) View from the rear ( X-Y plane)
Recall, (^) x
dR h dx
, (^) y
dR h dy
, and (^) z
dR h dz
is the distance from a fixed origin to a point P
Let the fixed origin be the apex (tip) of the cone. Here, let r 0 be the perpendicular distance from the Z -axis to the
body surface. Let r be the perpendicular distance from the Z -axis to point P. (Note that this is a different r than what
we defined previously for a general 3-D coordinate system. It is the same r , however, that we defined previously
when we discussed axisymmetric boundary layers.)
The boundary layer coordinates are ( x , y , z ) where x is a straight line along the body surface from the origin (a ray), y
Now, by definition,
2 2
x
dR X Y Z h dx x x x
, and similarly for the other scale factors, i.e.,
2 2
y
dR X Y Z h dy y y y
and
2 2
z
dR X Y Z h dz z z z
In class we will solve for these scale factors for this example. These can then be plugged into the 3-D boundary layer
equations.
Note : If we assume that the boundary layer is thin with respect to r 0 , and that there is no swirl, these equations should
reduce to the Mangler equations for axisymmetric flow!