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3-D Boundary Layer Cone - Foundations of Fluid Mechanics II - Lecture Notes, Study notes of Fluid Mechanics

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

Typology: Study notes

2012/2013

Uploaded on 10/03/2013

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Example of Scale Factors for 3-D Boundary Layer Equations – Flow over a Cone
Geometry
Y
r y
α
x
α
α
R
G
r0
P
Z
z or
θ
n
G
X X-Z plane
z or
θ
r0
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)
Definition of scale factors or stretching factors
Recall, x
dR
hdx
G
, y
dR
hdy
G
, and z
dR
hdz
G
, where
(
)
,,
R
XYZ
G
is the distance from a fixed origin to a point P
inside the boundary layer. Consider a simple cone of half-angle
α
as an example (axisymmetric about the Z-axis).
Let the fixed origin be the apex (tip) of the cone. Here, let r0 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
is normal to the body surface, and z is the angle along the body in the
θ
-direction, measured from the X-axis. (In fact,
we can let z =
θ
.) From trig, we see that X = rcos(
θ
), Y = rsin(
θ
), and Z = xcos(
α
) - ysin(
α
). Also, we see that r =
xsin(
α
) + ycos(
α
).
Now, by definition,
22
x
dR X Y Z
hdx x x x
∂∂
⎛⎞⎛⎞
≡= + +
⎜⎟⎜⎟
∂∂∂
⎝⎠⎝⎠
G2
, and similarly for the other scale factors, i.e.,
22
y
dR X Y Z
hdy y y y
⎛⎞⎛⎞
∂∂
≡= + +
⎜⎟⎜⎟
∂∂∂
⎝⎠⎝⎠
G2
and
22
z
dR X Y Z
hdz z z z
∂∂
⎛⎞⎛⎞
≡= + +
⎜⎟⎜⎟
∂∂∂
⎝⎠⎝⎠
2
G
.
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 r0, and that there is no swirl, these equations should
reduce to the Mangler equations for axisymmetric flow!
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Example of Scale Factors for 3-D Boundary Layer Equations – Flow over a Cone

Geometry

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)

Definition of scale factors or stretching factors

Recall, (^) x

dR h dx

G

, (^) y

dR h dy

G

, and (^) z

dR h dz

G

, where R ≡( X Y Z , , )

G

is the distance from a fixed origin to a point P

inside the boundary layer. Consider a simple cone of half-angle α as an example (axisymmetric about the Z -axis).

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

is normal to the body surface, and z is the angle along the body in the θ-direction, measured from the X -axis. (In fact,

we can let z = θ.) From trig, we see that X = r ⋅cos( θ), Y = r ⋅sin( θ), and Z = x ⋅cos( α) - y ⋅sin( α). Also, we see that r =

x ⋅sin( α) + y ⋅cos( α).

Now, by definition,

2 2

x

dR X Y Z h dx x x x

⎛ ∂^ ⎞ ⎛ ∂^ ⎞ ⎛ ∂ ⎞

⎝ ∂^ ⎠ ⎝ ∂^ ⎠ ⎝ ∂ ⎠

G 2

, and similarly for the other scale factors, i.e.,

2 2

y

dR X Y Z h dy y y y

⎝ ∂^ ⎠ ⎝ ∂^ ⎠ ⎝ ∂ ⎠

G 2

and

2 2

z

dR X Y Z h dz z z z

⎛ ∂^ ⎞ ⎛ ∂^ ⎞ ⎛ ∂ ⎞

⎝ ∂^ ⎠ ⎝ ∂^ ⎠ ⎝ ∂ ⎠

G 2

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!

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