The velocity field for steady inviscid flow from left to right over a circular cylinder, of radius R is given by V → = U cos θ [ 1 − ( R r ) 2 ] e ^ r − U sin θ [ 1 + ( R r ) 2 ] e ^ θ Obtain expressions for the acceleration of a fluid particle moving along the stagnation streamline ( θ = π ) and for the acceleration along the cylinder surface ( r = R ). Plot a r as a function of r = R for θ = π , and as a function of θ for r = R ; plot a θ as a function of θ for r = R . Comment on the plots. Determine the locations at which these accelerations reach maximum and minimum values.
The velocity field for steady inviscid flow from left to right over a circular cylinder, of radius R is given by V → = U cos θ [ 1 − ( R r ) 2 ] e ^ r − U sin θ [ 1 + ( R r ) 2 ] e ^ θ Obtain expressions for the acceleration of a fluid particle moving along the stagnation streamline ( θ = π ) and for the acceleration along the cylinder surface ( r = R ). Plot a r as a function of r = R for θ = π , and as a function of θ for r = R ; plot a θ as a function of θ for r = R . Comment on the plots. Determine the locations at which these accelerations reach maximum and minimum values.
Solution Summary: The author analyzes the acceleration of the particle moving along stagnation streamline and along the cylinder surface.
The velocity field for steady inviscid flow from left to right over a circular cylinder, of radius R is given by
V
→
=
U
cos
θ
[
1
−
(
R
r
)
2
]
e
^
r
−
U
sin
θ
[
1
+
(
R
r
)
2
]
e
^
θ
Obtain expressions for the acceleration of a fluid particle moving along the stagnation streamline (θ = π) and for the acceleration along the cylinder surface (r = R). Plot ar as a function of r = R for θ = π, and as a function of θ for r = R; plot aθ as a function of θ for r = R. Comment on the plots. Determine the locations at which these accelerations reach maximum and minimum values.
y
x = r cos 0
V = Or
y = r sine
r = √x² + y²
χ
Flow in "solid body rotation" acts like a solid spinning around an axis. The streamlines are circular,
the velocity is purely tangential, and the velocity magnitude is V = r, where is the angular
velocity (positive counter-clockwise) and r is the radius.
(a) Express the velocity vector V as a function of x and y.
(b) Calculate the curl of the velocity vector V × V, indicating clearly the direction of the resulting
vector.
A stream function is given by = 4x – 3y. The resultant velocity at any point is
1.6 An incompressible Newtonian fluid flows in the z-direction in space between two par-
allel plates that are separated by a distance 2B as shown in Figure 1.3(a). The length and
the width of each plate are L and W, respectively. The velocity distribution under steady
conditions is given by
JAP|B²
Vz =
2µL
B
a) For the coordinate system shown in Figure 1.3(b), show that the velocity distribution
takes the form
JAP|B?
v, =
2μL
Problems
11
- 2B --– €.
(a)
2B
(b)
Figure 1.3. Flow between parallel plates.
b) Calculate the volumetric flow rate by using the velocity distributions given above. What
is your conclusion?
2|A P|B³W
Answer: b) For both cases Q =
3µL
Chapter 5 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
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