BERNOULLI'S PRINCIPLE

: '''Bernoulli's equation' redirects here; see Bernoulli differential equation for an unrelated topic in ordinary differential equations.''
'Bernoulli's Principle' states that for an ideal fluid (low speed air is a good approximation), with no work being performed on the fluid, an increase in velocity occurs simultaneously with decrease in pressure or a change in the fluid's gravitational potential energy.
This principle is a simplification of Bernoulli's equation, which states that the sum of all forms of energy in a fluid flowing along an enclosed path (a streamline) is the same at any two points in that path. It is named after the Dutch/Swiss mathematician/scientist Daniel Bernoulli, though it was previously understood by Leonhard Euler and others. In fluid flow with no viscosity, and therefore, one in which a pressure difference is the only accelerating force, the principle is equivalent to Newton's laws of motion.

Contents

Incompressible flow

Compressible flow

Derivations of Bernoulli equation

Incompressible fluids

Compressible fluids

External links

References

Incompressible flow

The original form, for incompressible flow in a uniform gravitational field, is:
: $\{v^2\; over\; 2\}+gh+\{p\; over$
ho}=mathrm{constant}
where:
: ''v'' = fluid velocity along the streamline
: ''g'' = acceleration due to gravity
: ''h'' = height of the fluid
: ''p'' = pressure along the streamline
: ''$$
ho'' = density of the fluid
These assumptions must be met for the equation to apply:

★ Inviscid flow − viscosity (internal friction) = 0

★ Steady flow

★ Incompressible flow − $$
ho = constant along a streamline. Density may vary from streamline to streamline, however.

★ Generally, the equation applies along a streamline. For constant-density potential flow, it applies throughout the entire flow field.
An increase in velocity and the corresponding decrease in pressure, as shown by the equation, is often called Bernoulli's principle. The equation is named for Daniel Bernoulli although it was first presented in the above form by Leonhard Euler.
A common misconception used to illustrate the effect of Bernoulli's principle is when air flows around an airplane wing; the velocity of the air is described as being higher and the pressure is lower on the top surface of the wing when compared to the bottom surface, but this is easily invalidated. [1]
This can be rewritten as^[1]:
: $\{v^2$
ho over 2}+
ho g h+p=q+
ho g h+p=mathrm{constant}
where:
: ''q'' = dynamic pressure

Compressible flow

A second, more general form of Bernoulli's equation may be written for compressible fluids, in which case, following
a streamline:
: $\{v^2\; over\; 2\}+\; phi\; +\; w\; =mathrm\{constant\}$
:$phi\; ,$ = gravitational potential energy per unit mass, $phi\; =\; gh\; ,$ in the case of a uniform gravitational field
:$w\; ,$ = fluid enthalpy per unit mass, which is also often written as $h\; ,$ (which conflicts with the use of $h\; ,$ in this article for "height"). Note that
ho} where $epsilon\; ,$ is the fluid thermodynamic energy per unit mass, also known as the specific internal energy or "sie".
The constant on the right hand side is often called the Bernoulli constant and denoted $b$.
For steady inviscid adiabatic flow with no additional sources or sinks of energy, $b$ is constant along
any given streamline. More generally, when $b$ may vary along streamlines, it still
proves a useful parameter, related to the "head" of the fluid (see below).
When shock waves are present, in a reference frame moving with a shock, many of
the parameters in the Bernoulli equation suffer abrupt changes in passing through the shock. The
Bernoulli parameter itself, however, remains unaffected. An exception to this rule is radiative shocks, which
violate the assumptions leading to the Bernoulli equation, namely the lack of additional sinks or sources
of energy.

Derivations of Bernoulli equation

Incompressible fluids

The Bernoulli equation for incompressible fluids can be derived by integrating the Euler equations, or applying the law of conservation of energy in two sections along a streamline, ignoring viscosity, compressibility, and thermal effects.
The simplest derivation is to first ignore gravity and consider constrictions and expansions
in pipes that are otherwise straight, as seen in Venturi effect. Let the x axis be
directed down the axis of the pipe.
The equation of motion for a parcel of fluid on the axis of
the pipe is
:
:$$
ho A dx rac{dv}{dt}= -A dp
:$$
ho rac{dv}{dt}= -rac{dp}{dx}
In steady flow, $v=v(x)$ so
:
With $$
ho constant, the equation of motion can be written as
:
ho rac{v^2}{2} + p
ight) =0
or
:
ho}= C
where $C$ is a constant, sometimes referred to as the Bernoulli constant.
We deduce that where the speed is large, pressure is low. In the above derivation,
no external work-energy principle is invoked. Rather, the work-energy principle was
inherently derived by a simple manipulation of the momentum equation. The derivation that
follows includes gravity and applies to a curved trajectory, but a work-energy principle
must be assumed.

Applying conservation of energy in form of the work-kinetic energy theorem we find that:
:the change in KE of the system equals the net work done on the system;
:$W=Delta\; KE.\; ;$
Therefore,
:the work done by the forces in the fluid + decrease in potential energy = increase in kinetic energy.
The work done by the forces is
: $F\_\{1\}\; s\_\{1\}-F\_\{2\}\; s\_\{2\}=p\_\{1\}\; A\_\{1\}\; v\_$
{1}Delta t-p_{2} A_{2} v_{2}Delta t. ;
The decrease of potential energy is
: $m\; g\; h\_\{1\}-m\; g\; h\_\{2\}=$
ho g A
_{1} v_{1}Delta t h_{1}-
ho g A_{2} v_{2} Delta
t h_{2} ;
The increase in kinetic energy is
:
ho A_{2} v_{2}Delta t v_{2}
^{2}-rac{1}{2}
ho A_{1} v_{1}Delta t v_{1}^{2}.
Putting these together,
: $p\_\{1\}\; A\_\{1\}\; v\_\{1\}Delta\; t-p\_\{2\}\; A\_\{2\}\; v\_\{2\}Delta\; t+$
ho g A_{1} v_{1}Delta t h_{1}-
ho g A_{2} v_{2}Delta t h_{2}=rac{1}{2}
ho A_{2} v_{2}Delta t v_{2}^{2}-rac{1}{2}
ho A_{1} v_{1}Delta t v_{1}^{2}
or
:
ho A_{1} v_{1}Delta t v_{1}^{
2}}{2}+
ho g A_{1} v_{1}Delta t h_{1}+p_{1} A_{1
} v_{1}Delta t=rac{
ho A_{2} v_{2}Delta t v_{
2}^{2}}{2}+
ho g A_{2} v_{2}Delta t h_{2}+p_{2}
A_{2} v_{2}Delta t.
After dividing by $Delta\; t$, $$
ho and $A\_\{1\}\; v\_\{1\}$ (= rate of fluid flow = $A\_\{2\}\; v\_\{2\}$ as the fluid is incompressible):
:
ho}=rac{v_{2}^{2}}{2}+g h_{2}+rac{p_{2}}{
ho}
or, as stated in the first paragraph:
:
ho}=C
Further division by ''g'' implies
:
ho g}=C
A free falling mass from a height ''h'' (in vacuum), will reach a velocity
:$v=sqrt\{\{2\; g\}\{h\}\},$ or .
The term is called the ''velocity head''.
The hydrostatic pressure or ''static head'' is defined as
:$p=$
ho g h ,, or
ho g}.
The term
ho g} is also called the ''pressure head''.
A way to see how this relates to conservation of energy directly is to multiply by density and by unit volume (which is allowed since both are constant) yielding:
:$v^2$
ho + P = constant , and
:$mV^2\; +\; P\; cdot\; volume\; =\; constant\; ,$

Compressible fluids

The derivation for compressible fluids is similar. Again, the derivation depends upon (1) conservation of mass, and (2) conservation of energy.
Conservation of mass implies that in the above figure, in the interval of time $Delta\; t$, the amount
of mass passing through the boundary defined by the area $A\_1$ is equal to the
amount of mass passing outwards through the boundary defined by the area $A\_2$:
:$0\; =\; Delta\; M\_1\; -\; Delta\; M\_2\; =$
ho_1 A_1 v_1 , Delta t -
ho_2 A_2 v_2 , Delta t .
Conservation of energy is applied in a similar manner: It is assumed that the change in energy of the volume
of the streamtube bounded by $A\_1$ and $A\_2$ is due entirely to energy
entering or leaving through one or the other of these two boundaries. Clearly, in a more complicated situation
such as a fluid flow coupled with radiation, such conditions are not met. Nevertheless, assuming this to be
the case and assuming the flow is steady so that the net change in the energy is zero,
:$0\; =\; Delta\; E\_1\; -\; Delta\; E\_2\; ,$
where $Delta\; E\_1$ and $Delta\; E\_2$ are the energy entering through
$A\_1$ and leaving through $A\_2$, respectively.
The energy entering through $A\_1$ is the sum of the kinetic energy entering, the energy entering
in the form of potential gravitational energy of the fluid, the
fluid thermodynamic energy entering, and the energy entering in the form of mechanical $p,dV$ work:
:
ho_1 v_1^2 + phi_1
ho_1 + epsilon_1
ho_1 + p_1
ight] A_1 v_1 , Delta t
A similar expression for $Delta\; E\_2$ may easily be constructed.
So now setting $0\; =\; Delta\; E\_1\; -\; Delta\; E\_2$:
:
ho_1 v_1^2+ phi_1
ho_1 + epsilon_1
ho_1 + p_1
ight] A_1 v_1 , Delta t - left[ rac{1}{2}
ho_2 v_2^2 + phi_2
ho_2 + epsilon_2
ho_2 + p_2
ight] A_2 v_2 , Delta t
which can be rewritten as:
:
ho_1}
ight]
ho_1 A_1 v_1 , Delta t - left[ rac{1}{2} v_2^2 + phi_2 + epsilon_2 + rac{p_2}{
ho_2}
ight]
ho_2 A_2 v_2 , Delta t
Now, using the previously-obtained result from conservation of mass, this may be simplified to obtain
:
ho} = {
m constant} equiv b
which is the Bernoulli equation for compressible flow.

External links

★ Daniel Bernoulli and the making of the fluid equation the story of what happened.

★ Testing Bernoulli: a simple experiment here is an experiment that you can easily do yourself to test Bernoulli's equation. There are also 2 questions and answers.

★ Animated Demonstration of Bernoulli's Principle Adjustable animation of Bernoulli's principle with explanation and links.

★ Article on application of Bernoulli principle in F1 aerodynamic design Bernoulli in F1

★ The Bernoulli Effect and Vocal Fold Vibration Article describing how the Bernoulli principle causes the vocal folds to vibrate

★ Wikibooks Acoustics module on the Human Vocal Fold giving the mathematical model behind vocal fold vibration that uses the Bernoulli principle.

References

1. [2]