Understanding Stream Functions and Potential Functions in 2D Fluid Dynamics, Study notes of Aeronautical Engineering

Clarifications on the concepts of stream functions and potential functions in the context of 2d fluid dynamics. It covers topics such as mass flow, mass continuity equation, and the relationship between streamlines and stream function lines. It also explains the differences between various notations and their applications.

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2011/2012

Uploaded on 07/22/2012

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Lecture F12 Mud: Stream Function, Potential Function
(25 respondents)
¯ ¯
1. The book claims 2 = 1 represents mass flow perpendicular to the page”.
Isn’t 2-D flow in the plane of the page? (1 student)
It actually says “mass flow per unit depth perpendicular to the page”. The “perpen-
dicular” refers to the unit depth, not to the flow.
¯
2. What’s the difference between and ? (2 students)
¯
is the most general type of stream function, and gives the mass flux components:
¯ ¯
��/�y = �u �/� x = �v
For low speed flows where is a constant, it is convenient to absorb the constant
¯
factor into the stream function by defining = �/�. We now have:
��/�y = u �/�x = v
¯
It’s important to remember that can be used only for low speed flows, while has
no such restriction.
¯ ¯
The difference 2 1 gives the mass flow between two streamlines, while 2 1
gives the volume flow between two streamlines (but only in low-speed flow).
3. Where does (x, y) = ln x2 + y2 come from? (1 student)
I just made it up. The neat thing about a stream function is that no matter how
complicated (x, y) might get, the resulting u(x, y) and v(x, y) that you get from it
satisfy the mass continuity equation
ρ
V �u/�x + �v/�y = 0 ·
and hence represent a physically possible flow.
4. Is there are graphical relation between streamlines and stream function
lines? (1 student)
Lines of constant stream function are the same as streamlines.
5. I don’t understand how the funnel-shaped and the spiral-shaped repre-
sent the same vortex flow? (1 student)
Both functions produce the same u(x, y) and v(x, y), and hence they both represent
the same physical flowfield.
6. Will be dealing mostly with 2-D flows? (1 student)
The approach in Unified Fluids is to present concepts in the simplest way possible, so
that the understanding isn’t lost in unnecessary complexity. So we use the smallest
number of spatial dimensions in the examples and applications. Sometimes 1-D, usually
2-D, and occasionally 3-D if it’s unavoidable.
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Lecture F12 Mud: Stream Function, Potential Function

(25 respondents)

  1. The book claims “� 2

1

represents mass flow perpendicular to the page”.

Isn’t 2-D flow in the plane of the page? (1 student)

It actually says “mass flow per unit depth perpendicular to the page”. The “perpen

dicular” refers to the unit depth, not to the flow.

  1. What’s the difference between � and �? (2 students)

� is the most general type of stream function, and gives the mass flux components:

��/�y = �u − ��/�x = �v

For low speed flows where � is a constant, it is convenient to absorb the constant �

factor into the stream function by defining � = �/�. We now have:

��/�y = u − ��/�x = v

It’s important to remember that � can be used only for low speed flows, while � has

no such restriction.

The difference � 2

1

gives the mass flow between two streamlines, while � 2

1

gives the volume flow between two streamlines (but only in low-speed flow).

  1. Where does �(x, y) = ln

x

2

  • y

2 come from? (1 student)

I just made it up. The neat thing about a stream function is that no matter how

complicated �(x, y) might get, the resulting u(x, y) and v(x, y) that you get from it

satisfy the mass continuity equation

ρ � ·V � �u/�x + �v/�y = 0

and hence represent a physically possible flow.

  1. Is there are graphical relation between streamlines and stream function

lines? (1 student)

Lines of constant stream function are the same as streamlines.

  1. I don’t understand how the funnel-shaped � and the spiral-shaped ∂ repre

sent the same vortex flow? (1 student)

Both functions produce the same u(x, y) and v(x, y), and hence they both represent

the same physical flowfield.

  1. Will be dealing mostly with 2-D flows? (1 student)

The approach in Unified Fluids is to present concepts in the simplest way possible, so

that the understanding isn’t lost in unnecessary complexity. So we use the smallest

number of spatial dimensions in the examples and applications. Sometimes 1-D, usually

2-D, and occasionally 3-D if it’s unavoidable.

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  1. What’s the difference between � and ∂? (1 student)

They are alternative ways to define the velocity field u(x, y) and v(x, y). There are

important differences also. For example, � is usable only in 2-D, while ∂ easily extends

to 3-D with minimal complication.

  1. Is there a physical interpretation of �, �, ∂? (1 student)

psi has several interpretations: streamlines, mass flow, as presented in the notes. ∂ is

a bit harder to interpret.

  1. Why would we use � or ∂? (1 student)

When applicable, they almost always produce a tremendous mathematical simplifica

tion of a fluid flow problem. This makes solving the equations much easier and/or

faster.

  1. Are there conditions under which these methods work? (1 student)

Yes. The main restrictions are: � and � are usable only in 2-D

∂ is usable only for irrotational flows.

  1. Seems like we’re learning only endless equations and symbols. Where’s the

justification? (1 student)

So far we’ve focused almost entirely on “tools and concepts”. Applications will come

next. Anderson lays out this strategy.

  1. Can you give a numerical example of calculating a directional derivative?

(1 student)

A directional derivative is normally computed using the dot product.

�∂/�n = �∂ ·nˆ

For example, say

∂(x, y) = − arctan(y/x)

and we want to know �∂/�n at the point (x, y) = (0, 1), along a line tilted 45

� up from

horizontal. Along this direction

n ˆ = �

ˆı + �

ψˆ

and the gradient at the chosen point is

�∂ = 1 ˆı + 0 ˆψ

Hence,

�∂/�n = �∂ · n ˆ = �

  1. No mud (10 students)

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