Similarity Transformations in Fluid Mechanics
Similarity Transformations in Fluid Mechanics Similarity Transformations in Fluid Mechanics
Fluid Mechanics General Perspective and Application Department of Mathematics COMSATS Institute of Information Technology Islamabad Pakistan
- Page 2 and 3: • Archimedes(287-217 B.C.) observ
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- Page 7 and 8: The mass of a fluid in a control vo
- Page 9 and 10: ( uvw , , )andT If are velocity com
- Page 11 and 12: Diagram of a simple filtration Filt
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- Page 17 and 18: ∂ u = 0, v = 0 at y = 0, ∂y u =
- Page 19 and 20: References 1. Exact solutions using
- Page 21 and 22: Bolus move into the esophagus 360 D
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<strong>Fluid</strong> <strong>Mechanics</strong> General<br />
Perspective and Application<br />
Department of Mathematics<br />
COMSATS Institute of Information Technology<br />
Islamabad Pakistan
• Archimedes(287-217 B.C.) observed float<strong>in</strong>g objects<br />
on water and reasoned out the pr<strong>in</strong>ciple of bouncy.<br />
• Da V<strong>in</strong>ci(1452-1519) built the first chamber canal lock.<br />
• Castelli(1577-1644) stated the cont<strong>in</strong>uity pr<strong>in</strong>ciple for<br />
the river flow.<br />
• Torricelli(1608-1647) perfected the barometer.<br />
• Pascal(1623-1662) discover the scalar nature of<br />
pressure<br />
• Newton(1642-1727) developed the resistance law.<br />
• Bernoulli(1700-1782)developed developed energy<br />
equation for <strong>in</strong>viscid fluids
Physical science deal<strong>in</strong>g with the action of fluids at rest (fluid<br />
statics) or <strong>in</strong> motion (fluid dynamics), and their <strong>in</strong>teraction with<br />
flow devices and applications <strong>in</strong> eng<strong>in</strong>eer<strong>in</strong>g.<br />
The subject branches out <strong>in</strong>to sub-discipl<strong>in</strong>es such as:<br />
Aeronautics/Astronautics: Aircraft and missile aerodynamics,<br />
control hydraulics, gas-bear<strong>in</strong>g gyros, propeller, turbojet and<br />
rocket, satellites and cool<strong>in</strong>g system.<br />
Civil eng<strong>in</strong>eer<strong>in</strong>g: Pipe and channel flows, surface and ground<br />
water hydrology, w<strong>in</strong>d and water structure loads, lake and<br />
harbor tides, coastl<strong>in</strong>e flows, sediment transport, river flood<strong>in</strong>g<br />
and meander<strong>in</strong>g and water and water-water treatment.<br />
Physics: Magneto hydrodynamics, fusion devices, cryogenics<br />
and superconductivity.<br />
Astrophysics: Star and galaxy formation, and evolution,<br />
<strong>in</strong>terstellar gas dynamics, solar w<strong>in</strong>d and comet tails.
Mathematics: Solution of differential equations,<br />
boundary conditions, nonl<strong>in</strong>ear differential equations,<br />
dynamic analogies and computational fluid dynamics.<br />
Mechanical/ Nuclear eng<strong>in</strong>eer<strong>in</strong>g: Pumps and<br />
compressor, impulse and reaction turb<strong>in</strong>es, bear<strong>in</strong>g<br />
lubrication, heat exchangers, process control, fluid<br />
controls, cool<strong>in</strong>g system, electrochemical devices,<br />
Two-Phase flows and heat<strong>in</strong>g ventilation and air<br />
condition<strong>in</strong>g.<br />
Chemical, Petroleum eng<strong>in</strong>eer<strong>in</strong>g: Material transport,<br />
filter<strong>in</strong>g, heat transfer, mix<strong>in</strong>g and multiphase flow.<br />
Biophysics: Blood flow, artificial organs, breath<strong>in</strong>g<br />
aids, heart-lung mach<strong>in</strong>es, and artificial hearts, cellular<br />
mass transport, heat transfer, locomotion.<br />
Geophysics: Meteorology, oceanography, upper<br />
atmosphere, space, planetary atmospheres,<br />
geomagnetism, cont<strong>in</strong>ental drift, mantel convection<br />
and Glacier flows.
• Aerodynamics: deals with the motion of air and other<br />
gases, and their <strong>in</strong>teractions with bodies <strong>in</strong> motion<br />
such as lift and drag.<br />
• Hydraulics: application of fluid mechanics to<br />
eng<strong>in</strong>eer<strong>in</strong>g devices <strong>in</strong>volv<strong>in</strong>g liquids such as flow<br />
through pipes, weir and dam design<br />
• Geophysical fluid dynamics: fluid phenomena<br />
associated with the dynamics of the atmosphere and<br />
the oceans such as hurricane and weather systems<br />
• Bio-fluid mechanics: fluid mechanics <strong>in</strong>volved <strong>in</strong><br />
biophysical processes such as blood flow <strong>in</strong> arteries,<br />
and many others<br />
• Astrophysical <strong>Fluid</strong> Dynamics :the fluid mechanics<br />
of the sun, stars and other astrophysical objects
The mass of a fluid <strong>in</strong> a control volume rema<strong>in</strong>s<br />
conserved. This fact leads to establish a relation<br />
between the fluid density and fluid velocity at any<br />
po<strong>in</strong>t. Mathematical form of this relation is called<br />
equation of cont<strong>in</strong>uity<br />
Dρ<br />
∂ρ<br />
+ ρdiv( V ) = 0 or + div( ρV<br />
) = 0<br />
Dt<br />
∂t<br />
ρ<br />
If the density ( ) is constant (<strong>in</strong>compressible flow), Eq.<br />
(1) reduce to the simple equation:<br />
(1)<br />
divV = 0 (2)
The well known Navier-Stokes equations<br />
(momentum Equation) for unsteady, <strong>in</strong>compressible<br />
viscous fluid <strong>in</strong> rectangular coord<strong>in</strong>ate system are<br />
given by<br />
∂ ∂ ∂ ∂ ⎛∂ ∂<br />
+ u + v = − + ν ⎜ +<br />
∂t ∂x ∂y ρ ∂x ⎝∂x ∂y<br />
2 2<br />
u u u 1 p u u<br />
2 2<br />
∂ ∂ ∂ ∂ ⎛∂ ∂<br />
+ u + v =− + ν ⎜ +<br />
∂t ∂x ∂y ρ ∂x ⎝∂x ∂y<br />
2 2<br />
v v v 1 p v v<br />
D<br />
Dt<br />
2 2<br />
where is the material time derivative, ρ is the<br />
density, p is pressure, µ is the viscosity of fluid, g is<br />
acceleration due to gravity and v is the velocity vector.<br />
⎞<br />
⎟<br />
⎠<br />
⎞<br />
⎟<br />
⎠<br />
(3)<br />
(4)
( uvw , , )andT<br />
If are velocity components and the<br />
temperature of the fluid respectively, then the energy<br />
equation is given by:<br />
Φ<br />
DT<br />
Dt<br />
2<br />
= α∇ + Φ<br />
where is the dissipation function and is thermal<br />
diffusivity of the fluid.<br />
Φ =<br />
∂ ∂<br />
τ μ δ λ λ μ<br />
u u<br />
' = (<br />
i<br />
+<br />
i) + div v where 3 +2 =0<br />
ij<br />
ij<br />
∂x<br />
∂x<br />
(7)<br />
j<br />
j<br />
τ<br />
T<br />
'<br />
ij<br />
∂<br />
∂<br />
u<br />
x<br />
α<br />
i<br />
j<br />
(5)<br />
(6)
• Model<strong>in</strong>g of pulsat<strong>in</strong>g diaphragms<br />
• Sweet cool<strong>in</strong>g or heat<strong>in</strong>g<br />
• Isotope separation<br />
• Filtration<br />
• Paper manufactur<strong>in</strong>g<br />
• Irrigation<br />
• Gra<strong>in</strong> regression dur<strong>in</strong>g solid propellant<br />
combustion
Diagram of a simple<br />
filtration<br />
Filtration process <strong>in</strong><br />
kidneys
Cross-flow Microfiltration (MF) is a low pressure process for<br />
separation of larger size solutes from aqueous solutions us<strong>in</strong>g a<br />
semi-permeable membrane. This process is carried out by hav<strong>in</strong>g a<br />
process solution flow along a membrane surface under pressure.<br />
Particulate matter circulates through the membrane tube, clean<strong>in</strong>g the<br />
membrane tube surface while filtrate flows through the membrane
The channel has a width <strong>in</strong> the y-direction of h, a length<br />
<strong>in</strong> the z-direction of l, and a length <strong>in</strong> the x-direction,<br />
the direction of flow. There is a pressure drop along<br />
the length of the channel, so that the pressure<br />
gradient is constant<br />
From the cont<strong>in</strong>uity equation we have<br />
u=<br />
u( y)<br />
And the momentum equation takes the follow<strong>in</strong>g form<br />
2<br />
1 dp ⎛ d u ⎞<br />
0 = − + ν ⎜ ,<br />
2 ⎟<br />
ρ dx ⎝ dy ⎠<br />
u = at y = and y = h<br />
The boundary conditions are: 0 0<br />
(9)
y-axis<br />
a<br />
Porous wall<br />
y=a<br />
Geometry<br />
x-axis<br />
Porous wall<br />
y=-a<br />
A channel of rectangular cross section, one side of the<br />
cross section, represent<strong>in</strong>g the distance between the<br />
porous walls, is taken to be much smaller than the other.<br />
Both channel walls are taken to have equal permeability.<br />
Furthermore he considered steady state,<br />
<strong>in</strong>compressible, lam<strong>in</strong>ar, no external forces on the fluid<br />
and the suction/<strong>in</strong>jection velocity is <strong>in</strong>dependent of<br />
position.
Under the above assumptions the cont<strong>in</strong>uity and<br />
momentum equations reduce to the follow<strong>in</strong>g form<br />
∂u<br />
∂x<br />
∂v<br />
+ =<br />
∂y<br />
0,<br />
∂ ∂ ∂ ⎛∂ ∂<br />
u<br />
∂x ∂y ρ ∂x ⎝∂x ∂y<br />
2 2<br />
u u 1 p u u<br />
+ v =− + ν ⎜ +<br />
2 2<br />
∂ ∂ ∂ ⎛∂ ∂<br />
u<br />
∂x ∂y ρ ∂y ⎝∂x ∂y<br />
The appropriate boundary conditions are<br />
2 2<br />
v v 1 p v v<br />
+ v =− + ν ⎜ +<br />
2 2<br />
⎞<br />
⎟,<br />
⎠<br />
⎞<br />
⎟,<br />
⎠<br />
(10)<br />
(11)<br />
(12)<br />
uxy ( , ) = 0, vxy ( , ) = vw<br />
at y=± a,<br />
(13)<br />
∂ u = 0, v = 0 at y = 0,<br />
∂ y<br />
(14)<br />
u=0 at x=0. (15)
Let us consider the two-dimensional, unsteady,<br />
<strong>in</strong>compressible viscous fluid <strong>in</strong> an elongated<br />
rectangular channel bounded by two porous walls.<br />
The mass and momentum equations give<br />
∂u<br />
∂x<br />
∂v<br />
+ =0,<br />
∂y<br />
∂ ∂ ∂ ∂ ⎛∂ ∂<br />
⎜<br />
∂t ∂x ∂y ρ ∂x ⎝∂x ∂y<br />
2 2<br />
u u u 1 p u u<br />
+ u + v =− + ν +<br />
2 2<br />
2 2<br />
∂v ∂v ∂v 1 ∂p ⎛∂ v ∂ v⎞<br />
+ u + v =− + ν ⎜ + ,<br />
2 2 ⎟<br />
∂t ∂x ∂y ρ ∂y ⎝∂x ∂y<br />
⎠<br />
The appropriate boundary conditions are<br />
⎞<br />
⎟,<br />
⎠<br />
(16)<br />
(17)<br />
(18)<br />
u=0, v=-v<br />
w<br />
at y=a(t), (19)
∂ u = 0, v = 0 at y = 0,<br />
∂y<br />
u<br />
= 0 at x = 0. (20)<br />
y-axis<br />
Porous wall<br />
a(t)<br />
X-axis<br />
Porous wall<br />
y=a(t)<br />
y=a(t)<br />
Geometry of the bulk fluid motion
The govern<strong>in</strong>g equations are<br />
∂u<br />
∂x<br />
∂v<br />
+ =0,<br />
∂y<br />
∂ ∂ ∂ ∂ ⎛∂ ∂<br />
∂ ∂ ∂ ∂ ⎝∂ ∂<br />
2 2<br />
u u u 1 p u u νεu<br />
+ u + v =− + ν ⎜ +<br />
2 2⎟−<br />
t x y ρ x x y k<br />
∂ ∂ ∂ ∂ ⎛∂ ∂<br />
∂ ∂ ∂ ∂ ⎝∂ ∂<br />
2 2<br />
v v v 1 p v v νεv<br />
+ u + v =− + ν ⎜ +<br />
2 2 ⎟−<br />
t x y ρ y x y k<br />
Where ɛ is the porosity and k is the permeability.<br />
The appropriate boundary conditions are<br />
u=0,<br />
v=-v at y=a(t),<br />
w<br />
∂ u = 0, v = 0 at y = 0,<br />
∂y<br />
⎞<br />
⎠<br />
⎞<br />
⎠<br />
,<br />
,<br />
(21)<br />
(22)<br />
(23)<br />
(24)
References<br />
1. Exact solutions us<strong>in</strong>g symmetry methods and conservation laws for the<br />
viscous flow through expand<strong>in</strong>g–contract<strong>in</strong>g channels.<br />
S. Asghar, M. Mushtaq, A.H. Kara<br />
Applied Mathematical Modell<strong>in</strong>g,Volume 32, Issue 12, 2008.<br />
2. Application of Homotopy perturbation method to deformable channel<br />
with wall suction and <strong>in</strong>jection <strong>in</strong> a porous medium.<br />
M. Mahmood, M. A. Hussa<strong>in</strong>, S. Asgar, T. Hayat<br />
International Journal of Nonl<strong>in</strong>ear Sciences and Numerical Simulation.<br />
3. Application of Homotopy perturbation method to deformable channel with<br />
wall suction and <strong>in</strong>jection <strong>in</strong> a porous medium.<br />
M. Mahmood, M. A. Hussa<strong>in</strong>, S. Asgar, T. Hayat<br />
International Journal of Nonl<strong>in</strong>ear Sciences and Numerical Simulation.
• The flow of ur<strong>in</strong>e from the kidneys <strong>in</strong>to the<br />
bladder through tubular organs<br />
• Bile from the gallbladder <strong>in</strong>to the duodenum<br />
• Peristalsis pushes <strong>in</strong>gested food through the<br />
digestive tract towards its release at the<br />
anus<br />
• Worms propel themselves through peristaltic<br />
movement<br />
• Spermatic flow is also due to the peristalsis<br />
motion<br />
• Peristaltic pump
Bolus move <strong>in</strong>to the<br />
esophagus<br />
360 Degree Peristaltic Pump
The equations that govern the flow are the<br />
cont<strong>in</strong>uity equation and Navier Stokes equations<br />
The wall motion is described by:<br />
2<br />
hxt ( , ) = a+ bs<strong>in</strong> π ( x−ct)<br />
λ<br />
(25)<br />
b<br />
λ<br />
Coord<strong>in</strong>ate system and the channel under consideration
The govern<strong>in</strong>g equations are the cont<strong>in</strong>uity equation<br />
and Navier Stokes equations<br />
The wall motion is described by:<br />
2<br />
hxt ( , ) = at ( ) + bs<strong>in</strong> π ( x−ct)<br />
λ<br />
where the distance between the walls is chang<strong>in</strong>g <strong>in</strong> (26)<br />
time<br />
b<br />
λ<br />
Coord<strong>in</strong>ate system and the channel under consideration
References<br />
1. Peristaltic flow <strong>in</strong> a deformable channel.<br />
D. N. Khan Marwat, S. Asghar<br />
2. Application of Homotopy perturbation method to deformable<br />
channel with wall suction and <strong>in</strong>jection <strong>in</strong> a porous medium.<br />
M. Mahmood, M. A. Hussa<strong>in</strong>, S. Asgar, T. Hayat<br />
International Journal of Nonl<strong>in</strong>ear Sciences and Numerical<br />
Simulation.<br />
3. Application of Homotopy perturbation method to deformable<br />
channel with wall suction and <strong>in</strong>jection <strong>in</strong> a porous medium.<br />
M. Mahmood, M. A. Hussa<strong>in</strong>, S. Asgar, T. Hayat<br />
International Journal of Nonl<strong>in</strong>ear Sciences and Numerical<br />
Simulation.
• A cont<strong>in</strong>uously mov<strong>in</strong>g surface through a<br />
quiescent medium:<br />
• Hot roll<strong>in</strong>g, wire draw<strong>in</strong>g, sp<strong>in</strong>n<strong>in</strong>g of laments,<br />
metal extrusion, crystal grow<strong>in</strong>g, cont<strong>in</strong>uous<br />
cast<strong>in</strong>g, glass fiber production, and paper<br />
production.<br />
• The flow over a cont<strong>in</strong>uous material mov<strong>in</strong>g<br />
through a quiescent fluid is <strong>in</strong>duced by the<br />
movement of the solid material and by thermal<br />
buoyancy.<br />
• Cool<strong>in</strong>g of electronic devices
Cool<strong>in</strong>g of electronic devices<br />
CPU heat s<strong>in</strong>k with fan<br />
attached<br />
Radial isotherm and swirl<strong>in</strong>g<br />
forced convection flow<br />
trajectories
Mixed convection flow along a vertical<br />
stretch<strong>in</strong>g plate with variable plate<br />
temperature<br />
x<br />
Mixed convection flow<br />
along a heated<br />
cont<strong>in</strong>uously mov<strong>in</strong>g<br />
surface subject to nonuniform<br />
surface<br />
temperature assum<strong>in</strong>g<br />
that the surface velocity<br />
is u 0 x and the wall<br />
temperature is T 0 x 2 .<br />
u=U(x)<br />
v =0<br />
T w<br />
O<br />
u<br />
g<br />
v<br />
δ T<br />
T ∞<br />
δ<br />
u=0<br />
y
Boundary-layer equations<br />
Mak<strong>in</strong>g the usual boundary-layer approximations<br />
∂<br />
∂<br />
u<br />
x<br />
∂v<br />
+ =<br />
∂y<br />
0<br />
2<br />
u u u<br />
∂ ∂ ∂<br />
u + v = ν + g β ( T − T )<br />
2<br />
∞<br />
∂x ∂y ∂ y<br />
u<br />
2 2 3<br />
⎡ ∂ ⎛ ∂ u ⎞ ∂u ∂ v ∂ u<br />
+ K ⎢ ⎜ u<br />
2 ⎟ + + v<br />
2 3<br />
⎣ ∂x<br />
⎝ ∂y ⎠ ∂y<br />
∂y ∂y<br />
2<br />
T T T<br />
∂ ∂ ∂<br />
+ v = α<br />
∂x ∂y ∂ y<br />
2<br />
⎤<br />
⎥<br />
⎦<br />
(27)<br />
(28)<br />
(29)
Boundary conditions<br />
We have assumed that the flow is caused by the<br />
stretch<strong>in</strong>g of the wall and the buoyancy effect<br />
due to variable surface temperature<br />
u= U(), x v = 0, T= T +Δ T() x at y=<br />
0<br />
u→ 0, T= T as y→∞<br />
∞<br />
∞<br />
where T ∞ is the temperature of the ambient fluid.<br />
Here we consider the follow<strong>in</strong>g form of the<br />
surface temperature and the stretch<strong>in</strong>g velocity<br />
of the surface<br />
2<br />
0 0<br />
(30)<br />
Δ Tx () = Tx, Ux () = ux<br />
(31)
References<br />
1. Mixed convection flow of second grade fluid along a vertical stretch<strong>in</strong>g flat<br />
surface with variable surface temperature.<br />
M. Mushtaq, S. Asghar and M. A. Hossa<strong>in</strong><br />
Heat and Mass Transfer, Volume 43, Number 10 / August, 2007.<br />
2. Squeezed flow and heat transfer over a porous surface for viscous fluid.<br />
M. Mahmood, M.A. Hussa<strong>in</strong>, S.Asgar<br />
Heat and mass transfer .<br />
3. Hydro-magnetic squeezed flow of a viscous <strong>in</strong>compressible fluid past a<br />
wedge with permeable surface.<br />
M. Mahmood, M.A. Hussa<strong>in</strong>, S. Asgar,<br />
ZAMM.<br />
4. www.google.com.pk/images