FUNDAMENTALS of Fluid Mechanics (chapter 01)

CHAPTER 1
FUNDAMENTALS
1.1. INTRODUCTION
Man’s desire for knowledge of fluid phenomena began with his problems of water
supply, irrigation, navigation, and waterpower.
Matter exists in two states; the solid and the fluid, the fluid state being commonly
divided into the liquid and gaseous states. Solids differ from liquids and liquids from gases in
the spacing and latitude of motion of their molecules, these variables being large in a gas,
smaller in a liquid, and extremely small in a solid. Thus it follows that intermolecular
cohesive forces are large in a solid, smaller in a liquid, and extremely small in a gas.
1.2. DIMENSIONS AND UNITS
Dimension = A dimension is the measure by which a physical variable is expressed
quantitatively.
Unit = A unit is a particular way of attaching a number to the quantitative dimension.
Thus length is a dimension associated with such variables as distance, displacement,
width, deflection, and height, while centimeters or meters are both numerical units for
expressing length.
In fluid mechanics, there are only four primary dimensions from which all the
dimensions can be derived: mass, length, time, and force. The brackets around a symbol like
[M] mean “the dimension” of mass. All other variables in fluid mechanics can be expressed in
terms of [M], [L], [T], and [F]. For example, acceleration has the dimensions [LT-2
]. Force [F]
is directly related to mass, length, and time by Newton’s second law,
onAcceleratiMassForce
maF
×=
=
(1.1)
From this we see that, dimensionally, [F] = [MLT-2
].
1 kg-force = 9.81 Newton of force = 9.81 N
Prof. Dr. Atıl BULU1

Primary Dimensions in SI and MKS Systems
Primary Dimension MKS Units SI Units
Force [F] Kilogram (kg) Newton (N=kg.m/s2
)
Mass [M] M=G/g = (kgsec2
/m) Kilogram
Length [L] Meter (m) Meter (m)
Time [T] Second (sec) Second (sec)
Secondary Dimensions in Fluid Mechanics
Secondary Dimension MKS Units SI Units
Area [L2
] m2
m2
Volume [L3
] m3
m3
Velocity [LT-1
] m/sec m/sec
Acceleration [LT-2
] m/sec2
m/sec2
Pressure or stress
[FL-2
] = [ML-1
T-2
]
kg/m2
Pa= N/m2
(Pascal)
Angular Velocity [T-1
] sec-1
sec-1
Energy, work
[FL] = [ML2
T-2
]
kg.m J = Nm (Joule)
Power
[FLT-1
] = [ML2
T-3
]
kg.m/sec W = J/sec (Watt)
Specific mass (ρ)
[ML-3
] = [FT2
L-4
]
kg.sec2
/m4
kg/m3
Specific weight (γ)
[FL-3
] = [ML-2
T-2
]
Kg/m3
N/m3
Specific mass = ρ = The mass, the amount of matter, contained in a volume. This will
be expressed in mass-length-time dimensions, and will have the dimensions of mass [M] per
unit volume [L3
]. Thus,
Volume
Mass
ssSpecificMa =

[ ] ( )42
4
2
3
sec, mkg
L
FT
L
M
⎥
⎦
⎤
⎢
⎣
⎡
=⎥⎦
⎤
⎢⎣
⎡
=ρ
Specific weight= γ = will be expressed in force-length-time dimensions and will have
dimensions of force [F] per unit volume [L3
].
[ ] ( )3
223
, mkg
TL
M
L
F
Volume
Weight
ightSpecificwe
⎥
⎦
⎤
⎢
⎣
⎡
=⎥
⎦
⎤
⎢
⎣
⎡
=
=
γ
Because the weight (a force), W, related to its mass, M, by Newton’s second law of motion in
the form
MgW =
In which g is the acceleration due to the local force of gravity, specific weight and specific
mass will be related by a similar equation,
gργ = (1.2)
EXAMPLE 1.1: Specific weight of the water at 4o
C temperature is γ = 1000 kg/m3
.
What is its the specific mass?
SOLUTION:
( )
( )42
3
sec94.101
81.9
1000
1000
mkg
mkgg
==
==
ρ
ργ
EXAMPLE 1.2: A body weighs 1000 kg when exposed to a standard earth gravity
g = 9.81 m/sec2
. a) What is its mass? b) What will be the weight of the body be in Newton if
it is exposed to the Moon’s standard acceleration gmoon = 1.62 m/sec2
? c) How fast will the
body accelerate if a net force of 100 kg is applied to it on the Moon or on the Earth?
SOLUTION:
a) Since,
( )
( )42
sec94.101
81.9
1000
1000
mkg
g
W
M
kgmgW
===
==
b) The mass of the body remains 101.94 kgsec2
/m regardless of its location. Then,

( )kgmgW 14.16562.194.101 =×==
In Newtons,
( )Newton162081.914.165 =×
c) If we apply Newton’s second law of motion,
( )
( )2
sec98.0
94.101
100
100
ma
kgmaF
==
==
This acceleration would be the same on the moon or earth or anywhere.
All theoretical equations in mechanics (and in other physical sciences) are
dimensionally homogeneous, i.e.; each additive term in the equation has the same dimensions.
EXAMPLE 1.3: A useful theoretical equation for computing the relation between the
pressure, velocity, and altitude in a steady flow of a nearly inviscid, nearly incompressible
fluid is the Bernoulli relation, named after Daniel Bernoulli.
gzVpp ρρ ++= 2
0
2
1
Where
p0 = Stagnation pressure
p = Pressure in moving fluid
V = Velocity
ρ = Specific mass
z = Altitude
g = Gravitational acceleration
a) Show that the above equation satisfies the principle of dimensional homogeneity,
which states that all additive terms in a physical equation must have the same
dimensions. b) Show that consistent units result in MKS units.
SOLUTION:
a) We can express Bernoulli equation dimensionally using brackets by entering the
dimensions of each term.
[ ] [ ] [ ] [ ]gzVpp ρρ ++= 2
0
2
1
The factor ½ is a pure (dimensionless) number, and the exponent 2 is also dimensionless.

[ ] [ ] [ ][ ] [ ][ ][ ]
[ ] [ ]22
242224222
−−
−−−−−−
=
++=
FLFL
LLTLFTTLLFTFLFL
For all terms.
b) If we enter MKS units for each quantity:
( ) ( ) ( )( ) ( )( )( )mmmkgmmkgmkgmkg 242224222
secsecsecsec ++=
( )2
mkg=
Thus all terms in Bernoulli’s equation have units in kilograms per square meter when
MKS units are used.
Many empirical formulas in the engineering literature, arising primarily from
correlation of data, are dimensional inconsistent. Dimensionally inconsistent equations,
though they abound in engineering practice, are misleading and vague and even dangerous, in
the sense that they are often misused outside their range of applicability.
EXAMPLE 1.4: In 1890 Robert Manning proposed the following empirical formula
for the average velocity V in uniform flow due to gravity down an open channel.
2
1
3
21
SR
n
V =
Where
R = Hydraulics radius of channel
S= Channel slope (tangent of angle that bottom makes with horizontal)
n = Manning’s roughness factor
And n is a constant for a given surface condition for the walls and bottom of the channel. Is
Manning’s formula dimensionally consistent?
SOLUTION: Introduce dimensions for each term. The slope S, being a tangent or
ratio, is dimensionless, denoted by unity or [F0
L0
T0
]. The above equation in dimensional form
[ ]0003
21
TLFL
nT
L
⎥⎦
⎤
⎢⎣
⎡
⎥
⎦
⎤
⎢
⎣
⎡
=⎥
⎦
⎤
⎢
⎣
⎡
This formula cannot be consistent unless [L/T] = [L1/3
/T]. In fact, Manning’s formula is
inconsistent both dimensionally and physically and does not properly account for channel-
roughness effects except in a narrow range of parameters, for water only.

Engineering results often are too small or too large for the common units, with too
many zeros one way or the other. For example, to write F = 114000000 ton is long and
awkward. Using the prefix “M” to mean 106
, we convert this to a concise F = 114 Mton
(megatons). Similarly, t = 0.000003 sec is a proofreader’s nightmare compared to the
equivalent t = 3 μsec (microseconds)
TABLE 1.1
CONVENIENT PREFIXES FOR ENGINEERING UNITS
Multiplicative Factor Prefix Symbol
1012
tera T
109
giga G
106
mega M
103
kilo k
10 deka da
10-1
deci d
10-2
centi c
10-3
milli m
10-6
micro μ
10-9
nano n
10-12
pico p
10-15
femto f
10-18
atto a
1.3 MOLECULAR STRUCTURE OF MATERIALS
Solids, liquids and gases are all composed of molecules in continuous motion.
However, the arrangement of these molecules, and the spaces between them, differ, giving
rise to the characteristics properties of the three states of matter. In solids, the molecules are
densely and regularly packed and movement is slight, each molecule being strained by its
neighbors. In liquids, the structure is loser; individual molecules have greater freedom of
movement and, although restrained to some degree by the surrounding molecules, can break
away from the restraint, causing a change of structure. In gases, there is no formal structure,
the spaces between molecules are large and the molecules can move freely.
In this book, fluids will be assumed to be continuous substances, and, when the
behavior of a small element or particle of fluid is studied, it will be assumed that it contains so
many molecules that it can be treated as part of this continuum. Quantities such as velocity
and pressure can be considered to be constant at any point, and changes due to molecular
motion may be ignored. Variations in such quantities can also be assumed to take place
smoothly, from point to point.

1.4. COMPRESSIBILITY: BEHAVIOR OF FLUIDS AGAINST PRESSURE
For most purposes a liquid may be considered as incompressible. The compressibility
of a liquid is expressed by its bulk modulus of elasticity. The mechanics of compression of a
fluid may be demonstrated by imagining the cylinder and piston of Fig.1.1 to be perfectly
rigid (inelastic) and to contain a volume of fluid V. Application of a force, F, to piston will
increase the pressure, p, in the fluid and cause the volume decrease –dV. The bulk modulus of
elasticity, E, for the volume V of a liquid
VdV
dp
E −= (1.3)
V
dv
F
A
Fig. 1.1
Since dV/V is dimensionless, E is expressed in the units of pressure, p. For water at
ordinary temperatures and pressures, E = 2×104
kg/cm2
.
For liquids, the changes in pressure occurring in many fluid mechanics problems are
not sufficiently great to cause appreciable changes in specific mass. It is, therefore, usual to
ignore such changes and to treat liquids as incompressible.
ρ = Constant
1.5. VISCOSITY: BEHAVIOR OF FLUIDS AGAINST SHEAR STRESS
When real fluid motions are observed carefully, two basic types of motion are seen.
The first is a smooth motion in which fluid elements or particles appear to slide over each
other in layers or laminae; this motion is called laminar flow. The second distinct motion that
occurs is characterized by a random or chaotic motion of individual particles; this motion is
called turbulent flow.
Now consider the laminar motion of a real fluid along a solid boundary as in Fig. 1.2.
Observations show that, while the fluid has a finite velocity, u, at any finite distance from the
boundary, there is no velocity at the boundary. Thus, the velocity increases with increasing
distance from the boundary. These facts are summarized on the velocity profile, which
indicates relative motion between adjacent layers. Two such layers are showing having
thickness dy, the lower layer moving with velocity u, the upper with velocity u+du. Two
particles 1 and 2, starting on the same vertical line, move different distances d1 = udt and
d2 = (u+du) dt in an infinitesimal time dt.

dy
dυ
υdt
2 (υ + dυ)dt
2
1
dy
dy
Fig. 1.2
It is evident that a frictional or shearing force must exist between the fluid layers; it
may be expressed as a shearing or frictional stress per unit of contact area. This stress,
designated by τ, has been found for laminar (nonturbulent) motion to be proportional to the
velocity gradient, du/dy, with a constant of proportionality, μ, defined as coefficient of
viscosity or dynamic viscosity. Thus,
dy
du
μτ = (1.4)
All real fluids possess viscosity and therefore exhibit certain frictional phenomena
when motion occurs. Viscosity results fundamentally from cohesion and molecular
momentum exchange between fluid layers and, as flow occurs, these effects appear as
tangential or shearing stresses between the moving layers. This equation is called as Newton’s
law of viscosity.
Because Equ. (1.4) is basic to all problems of fluid resistance, its implications and
restrictions are to be emphasized:
1) The nonappearance of pressure in the equation shows that both τ and μ are
independent of pressure, and that therefore fluid friction is different from that between
moving solids, where plays a large part,
2) Any shear stress τ, however small, will cause flow because applied tangential forces
must produce a velocity gradient, that is, relative motion between adjacent fluid
layers,
3) Where du/dy = 0, τ = 0, regardless of the magnitude of μ, the shearing stress in
viscous fluids at rest will be zero,
4) The velocity profile cannot be tangent to a solid boundary because this would require
an infinite velocity gradient and infinite shearing stress between fluids and solids,
5) The equation is limited to nonturbulent (laminar) fluid motion, in which viscous action
is strong.
6) The velocity at a solid boundary is zero, that is, there is no slip between fluid and solid
for all fluids that can be treated as a continuum.

Shear - thickening fluid
Shear - thinning fluid
Newtonian fluid
Real plastic
Ideal ( Bingham ) plastic
Rate of strain , dυ/dy
τ
τ
1
1
Shearstress,τ
Fig. 1.3
Equ. (1.4) may be usefully visualized on the plot of Fig.1.3 on which μ is the slope of
a straight line passing through the origin, here du will be considered as displacement per unit
time and the velocity gradient du/dy as time of strain. Fluids that follow Newton’s viscosity
law are commonly known as Newtonian fluids. It is these fluids with which this book is
concerned. Other fluids are classed as non-Newtonian fluids. The science of Rheology, which
broadly is the study of the deformation and flow of matter, is concerned with plastics, blood,
suspensions, paints, and foods, which flow but whose resistance is not characterized by Equ.
(1.4).
The dimensions of the (dynamic) viscosity μ may be determined from dimensional
homogeneity as follows:
[ ] [ ]
[ ]
[ ]
[ ] [ ]TFL
LLT
FL
dydu
2
11
2
−
−−
−
===
τ
μ , )sec.( 2
mkg
In SI units, (Pa×sec). These combination times 10-1
is given the special name poises.
Viscosity varies widely with temperature. The shear stress and thus the viscosity of
gases will increase with temperature. Liquid viscosities decrease as temperature rises.
Owing to the appearance of the ratio μ/ρ in many of the equations of the fluid flow,
this term has been defined by,
ρ
μ
ϑ = (1.5)
in which υ is called the kinematic viscosity. Dimensional considerations of Equ. (1.5) shows
the units of υ to be square meters per second, a combination of kinematic terms, which
explains the name kinematic viscosity. The dimensional combination times 10-4
is known as
stokes.

1.6.VAPOR PRESSURE AND CAVITATION
Vapor pressure is the pressure at which a liquid boils and is in equilibrium with its
own vapor. For example, the vapor pressure of water at 100
C is 0.125 t/m2
, and at 400
C is
0.75 t/m2
. If the liquid pressure is greater than the vapor pressure, the only exchange between
liquid and vapor is evaporation at the interface. If, however, the liquid pressure falls below the
vapor pressure, vapor bubbles begin to appear in the liquid. When the liquid pressure is
dropped below the vapor pressure due to the flow phenomenon, we call the process
cavitation. Cavitation can cause serious problems, since the flow of liquid can sweep this
cloud of bubbles on into an area of higher pressure where the bubbles will collapse suddenly.
If this should occur in contact with a solid surface, very serious damage can result due to the
very large force with which the liquid hits the surface. Cavitation can affect the performance
of hydraulic machinery such as pumps, turbines and propellers, and the impact of collapsing
bubbles can cause local erosion of metal surfaces.

FUNDAMENTALS of Fluid Mechanics (chapter 01)

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