Superposition of Basic Plane Potential Flows | AME 30331, Study notes of Fluid Mechanics

Material Type: Notes; Professor: Sucosky; Class: Fluid Mechanics; Subject: Aerospace and Mechanical Engr.; University: Notre Dame; Term: Fall 2009;

Typology: Study notes

Pre 2010

Uploaded on 02/25/2010

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AME 30331 Fall 09
SUPERPOSITION OF BASIC PLANE POTENTIAL FLOWS
Source in uniform stream
Combined velocity potential and streamfunction
Uniform flow
Source
Streamfunction
Uy
2
m

Velocity potential
Ux
ln
2
mr

Therefore, the combination of a uniform flow and a doublet is expressed in cylindrical
coordinates as:
Streamfunction:
Velocity potential:
Velocity field
and
r
v
pf3
pf4
pf5
pf8
pf9
pfa

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SUPERPOSITION OF BASIC PLANE POTENTIAL FLOWS

Source in uniform stream

 Combined velocity potential and streamfunction

Uniform flow Source

Streamfunction^   Uy

m

Velocity potential   Ux ln

m

r

Therefore, the combination of a uniform flow and a doublet is expressed in cylindrical coordinates as:

Streamfunction:

Velocity potential:

 Velocity field

v r r

and v

 r

vr

v  

The velocity magnitude is:

V^2 

 Stagnation point

At b along the x-axis, the velocity of the flow due to the source cancels that due to the uniform flow.

at rb and  : vr

v  

vr ( rb ,   )  0 

 Equation of the streamline passing through the stagnation point

At the stagnation point:

 

Therefore, the streamline equation through the stagnation point is:

Doublet

A doublet is the combination of a source and sink

 Combined velocity potential and streamfunction

Sink Source

Streamfunction

m

  

m

Velocity potential ln

m

r

  ln

m

r

Therefore, the combination of a uniform flow and a doublet is expressed in cylindrical coordinates as:

Streamfunction:

Velocity potential:

From the combined streamfunction:

Using the identity  1 2  1 2 1 2

tan tan

tan

1 tan tan

, the expression can be rewritten:

where:

tan   1

tan   2

Therefore:

tan  1  2 

The streamfunction is obtained by taking the inverse tangent:

The expression above is the streamfunction for the combination of a source and a sink.

A doublet is obtained as m  , a  0 and

ma

K

Therefore, the streamfunction and velocity potential for a doublet can be expressed as:

where K is the strength of the doublet

Flow around a circular cylinder

The flow around a circular cylinder can be represented by combining a doublet with a uniform flow.

 Combined velocity potential and streamfunction

Uniform flow Doublet

Streamfunction^   Uy

K sin

r

Velocity potential   Ux

K cos

r

Therefore, the combination of a uniform flow and a doublet is expressed in cylindrical coordinates as:

Streamfunction:

Velocity potential:

 Boundary condition

In order to represent a cylinder of radius a , the perimeter of the cylinder must be a streamline in

the flow. Therefore, the streamfunction must be constant along the perimeter of the cylinder.

 Streamfunction and velocity potential of flow around a circular cylinder of radius a

Streamfunction:

Velocity potential:

 Velocity field The velocity field can be derived using the definition of the streamfunction in cylindrical coordinates:

v r r

 

and v

 r

vr

v  

Points where the maximum velocity is attained on the surface of the cylinder:

at ra : vr

v  

v max

Circulatory flow around a cylinder in a uniform stream

Circulatory flow around a cylinder in a uniform stream can be obtained by combining a vortex, a uniform flow and a doublet (i.e., a vortex and a flow around a cylinder)

 Combined velocity potential and streamfunction

Vortex Flow around cylinder

Streamfunction^ ^2  ln r

2

1 2 sin

a

Ur

r

Velocity potential 2 ^ 

2

1 2 cos

a

Ur

r

where is the circulation.

Therefore, the streamfunction and velocity potential for the circulatory flow around a cylinder in a uniform stream can be written:

Streamfunction:

Velocity potential:

 Velocity field

v r r

and v

 r

vr

v  

 Stagnation points on the cylinder

Stagnation points are points where the velocity is zero.

at ra : vr

v  

v  (^) ( ra )  0 

Therefore, the number of stagnation points on the cylinder depends on the value of .