Ideal Fluids in Motion, Study notes of Law

If a fluid is incompressible, its density ρ is constant throughout. Thus the volume of fluid entering a tube at one end per unit of time.

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R. Field 10/30/2012
University of Florida PHY 2053 Page 1
Ideal Fluids in Motion
2
2
2
2
1
21
2
1
2
1
1
gyvPgyvP
ρρρρ
++=++
)()()(
12
2
1
2
2
2
1
21
yyMgvvM
M
PP +=
ρ
Bernoulli’s Equation:
The Equation of Continuity:
Steady Flow, Incompressible Flow, Non viscous Flow, Irrotational Flow.
If a fluid is incompressible, its density ρ
ρρ
ρis constant throughout.
Thus the volume of fluid entering a tube at one end per unit of time
must be equal to the volume of fluid leaving the other end per unit
time. In the time
t we have A
1
v
1
t = A
2
v
2
t.
Ideal Fluid:
A
1
v
1
= A
2
v
2
(continuity equation) R
V
= Av = volume flow rate = constant
R
m
= ρ
ρρ
ρR
V
= ρ
ρρ
ρAv = mass flow rate = constant
Application of W =
KE +
U:
V = v
1
A
1
t
V = v
2
A
2
t
F
1
= P
1
A
1
ρ
M
PPVPPxAPxAPW )()()()(
2121222111
===
F
2
= P
2
A
2
M
M
x
2
= v
2
t
x
1
= v
1
t
pf3
pf4

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R. Field 10/30/2012University of Florida

PHY 2053

Page 1

Ideal Fluids in Motion

2

(^22) 1 2 2 1

(^21) 1 2 1

gy

v

P

gy

v

P

ρ

ρ

ρ

ρ^

(^

1 2

(^21) (^22)

1 2

2 1

y

y

Mg

v

v

M

M

P

P^

ρ

-^

Bernoulli’s Equation:

-^

The Equation of Continuity:

Steady Flow, Incompressible Flow, Non viscous Flow, Irrotational Flow. If a fluid is incompressible, its density

ρρρρ^

is constant throughout.

Thus the volume of fluid entering a tube at one end per unit of timemust be equal to the volume of fluid leaving the other end per unittime. In the time

t we have A

v 1

t = A

v 2

t.

-^

Ideal Fluid:

A^1

v^1

= A

v 2

(continuity equation) 2

RV

= Av = volume flow rate = constant

Rm

ρρρρ

RV

ρρρρ Av

mass flow rate = constant

Application of W =

KE +

U:

∆∆∆∆ V = v

A 1 ∆∆∆∆ t 1

∆∆∆∆ V = v

A 2 ∆∆∆∆ t 2

F^1

= P

A 1

M^ ρ 1 P P V P P x A P x

AP

W

(^

2 1 2 1 2 2 2 1 1 1 − = ∆ − = ∆ − ∆

=^

F^2

= P

A 2 2

M

M ∆∆∆∆ x

= v 2

∆∆∆∆ 2 t

∆∆ x ∆∆

= v 1

∆∆∆∆ 1 t

R. Field 10/30/2012University of Florida

PHY 2053

Page 2

Bernoulli’s Equation:

Applications

2

(^22) 1 2 2 1

(^21) 1 2 1

gy

v

P

gy

v

P

ρ

ρ

ρ

ρ^

gh

A ghA

v^

A A^

2

)) / ( (^1) (

2

1 2 (^21) 2

2

 

− =^

<<

-^

Bernoulli’s Equation:

-^

Constant Height (y

= y 1

If the speed of a fluid element increases as the element travelsalong a horizontal streamline, the pressure of the fluid mustdecrease, and conversely.

P + ½

ρρρρ v

ρρρρ gy = constant (conservation of energy for a fluid)

v^1

P^1 Air Foil

v^1

>> v

2 v^2

P^2

P^1

<< P

2

v^1

= v

A 2

/A 2

1

gh

v

v^

(^21) 2 2

P^1

= P

= P 2

atm

(^22) 1 2 2 (^21) 1 2 1

v

P

v

P

ρ

ρ^

P + ½

ρρρρ v

2 = constant

-^

Example (velocity of efflux):

y-axis

y = 0

h

v^2

ρρρρ

v^1

Area A

1

Area A

2

We can use Bernoulli’s equation to calculate the speed ofefflux, v

, from a horizontal orifice (and area A 2

) located a 2

depth h below the water level of a large talk (with area A

2

(^22) 1 2 2 1

(^21) 1 2 1

gy

v

P

gy

v

P

ρ^

=

(Torricelli’s Law)

)

(^

(^22) (^21) 1 2 1 2

v v

P P P^

= − = ∆

R. Field 10/30/2012University of Florida

PHY 2053

Page 4

Bernoulli’s Equation:

Application

)

( 2

h^2 d g

v^

=

-^

Siphon:

The figure shows a siphon, which is a device forremoving liquid from a container. Tube ABC mustinitially be filled, but once this is done, liquid willflow until the liquid surface of the container islevel with the tube opening A. With what speeddoes the liquid emerge from the tube at C? Whatis the greatest possible height h

that a siphon can 1

lift water?

gd

v

P

V

P^

A

atm

ρ^

=

+^

2 1 2

2 1 2

A va V

va

VA

/

=^ gd

v

P

gd

a A

v

P

P^

A A a

A

atm

ρ^

 → 

−

^ 

=^

<<

2 1 2

2 2

2 1 2

1

y=

V

v

v

A = Area of containera = area of tube

)

(^

2

2 1 2

2 1 2

h d g

v

P

gd

v

P^

atm

A^

  • − + = − +

)

(^

2

2 1 2

h d g

v^

=

ρ^

)

(^

2

2 1 2

1

2 1 2

h d g

v

P

gh

v

P^

atm

B^

  • − + = + +

)

(

) (^

2

max 1

h d

g P

h^

atm

=

ρ

)

( )

(^

2

1

h d

g P

P

h^

B

atm

=