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Fluid Mechanics Abdusselam Altunkaynak

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(1)

Fluid Mechanics

Abdusselam Altunkaynak

(2)

Potential Function

Potential function is a function where

It is a function which satisfies and

This function is only available in irrotational flows

Irrotational flow

(3)

in this equation

Substituting and

(4)

It has seen that the velocity components are

derived from the potential function

Since

Because of this in irrotational flows, velocity potential

motions are called potential flows in short

(5)

In all physically possible flows

(6)

For this definition to be true in reality the continuity

equation should be satisfied

Along the same flow line, the flow

function has the same value

In reality

(7)
(8)

We can prepare streamlines

by drawing the lines graphically

In potential flow the circulation which is defined as the integral

velocity along a closed curve should be zero.

We know that

So by equating the flow function to different constant values

k

(9)

Substituting k into

Therefore

(10)

Basic Equations of Potential Flows

The continuity equation and equation of motion

developed for 2-D ideal flows are the same with in

potential flow conditions

But we will treat the energy equation differently here

For a 2-D flow of x-y plane the two components of

Euler’s equations of motion were developed as

(11)

Adding these two equations we will get

By using the exact differential notion

calculus and algebra we end up with

This equation is Bernoulli’s equation. It is the energy

equation for ideal and permanent flows

(12)

If we check the irrotationality conditions for

potential flows

and

into the equation

Substituting

(13)

yields

This shows that the flow function satisfies the Laplace

equation in irrotational flow conditions

In potential flows, the potential function is given as

and

(14)

Substituting velocity definitions in the continuity equation

This shows that the potential function

The continuity equation for 2D flows is

(15)

In a certain potential flow

The streamlines and the iso-potential lines are

orthogonal to each other

We call this net created as a result of streamlines and

iso-potential lines, which are crossing each other

perpendicularly a Flow Net

If we draw these orthogonal lines, there will be a net formed

(16)

Since

(17)

In the same manner

(18)

Problems related to potential flows can be solved

graphically using this flow net

By using stream function velocity potential or both

We can understand that the streamlines and the iso-potential

lines are orthogonal to each other

We can determine velocity pressure

etc…at any point in the flow

For example we can analyze the nature of

(19)

Two Dimensional Flow of Real Fluids

Basic Equations

Continuity Equation

The continuity equation for 2-D real flows is given as

If is constant the continuity equation

will have the following form

(20)

Equation of motion

In the X-direction

In the Y-direction

Since the flow is real flow viscous forces are present

In this regard for 2-D real flow the equation of motions in two directions (x and y) are given as follows

(21)

If we assume the volumetric force to act only in one

direction i.e. vertically and solve the Navier-Stokes equation

is the head loss as a result of frictional (viscous) forces

we will get

(22)

Navier-Stokes equation can be used to solve problems

related to 2-D real fluids

Since the flow condition is hydrostatic, all velocity components are zero

We have to determine the value of C by taking boundary conditions

However the theoretical solution of Navier-Stokes equation is

possible in some special conditions

By solving Navier-Stokes equations we end up with

(23)

In conditions when we have infinitely large dimensions, the

flow between two plates is considered to be uniform and

permanent and therefore laminar

In this condition, the Navier-Stokes equations for 2-D flows

are written as follows

(24)

If we take only the component of the equation in the X-

direction, the component in the direction where the weigh is

not action for the given uniform and permanent flow

We have to use boundary conditions to find C1 and C2

we end up with

(25)

This is the parabolic velocity distribution equation developed

using the Navier-Stokes equation

Note:

is always negative. As a result, for the velocity to be

positive, we have to add a negative sign in front of .

(26)

Thanks to

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