CIRCULATION (CONT...)
CDEEP IIT Bombay
di' , v+ —y ay
CE 223 L f l /Slide
1) C
av , , + —ax
ax + —ay ay
an + —
Oy dy
11
dv
Ott U — dx + — dy ax ay
On ,
U —dx
ax
v + —0v
dx
V
Circulation around an elemental area
A B
CDEEP IIT Bombay IRROTATIONAL MOTION
CE 223 Lth/Slide.2_
Ferris Wheel
Fluid particles not rotating
--- --
.4P• •-•
h-rotational outer flow region
Velocity profile •
Rotational boundary layer region
7A-C■
"wit iStM-14(4k4.
Fluid particles rotating Wan
ROTATIONAL AND IRROTATIONAL FLOW
NEAR A WALL
CDEEP IIT Bombay
CE223 L I I 'Slid° •
Fluid elements in a rotational region of the flow rotate, but
those in an irrotational region of flow do not (souRea: car-tGaL cimsALA,2006)
VORTEX MOTION CDEEP
IIT Bombay
CE 223 L_UlSlide.
(a )
(b)
Streamlines and velocity profiles for flow A akin to solid body rotation, and flow B is irrotational everywhere except at the origin
z
4- Sz 1k
&Sy w
pzi8 yt5z pm+ —5x)5y5z
manly
CONTINUITY EQUATION
WEEP IIT Bombay
CE 223 L I I iSlide_5-
CONTINUITY EQUATION (CONTD)
CDEEP IIT Bombay
• The rate at which mass flows into the control CF 223 I IL/Slidell
volume, minus the rate at which the flow leaves the control volume must equal the net rate of change of mass within the control volume
a(pu) a(pv) „ a(pw) a. Sy
a(p Sr gy (5z) &Sy bz' by hi az z & =
at ay aZ at
CONTINUITY EQUATION (CONTD)
Divide right through by the volume (bx by bz), to arrive at the continuity equation in Cartesian
Op i_3(pu) a(pv) a(pw) =0 coordinates ox ay
CDEEP IIT Bombay
CE 223 1_ I I /Slide?
For incompressible flows, p is a constant and above can be
simplified as Cu ay au,
0 —+—+ — = ax "ay az
In case of steady compressible flows, the continuity equation
in the differential form is
a(pm) + a( pv) ± a(pw) =0
av tly az
STREAM FUNCTION
CDEEP IIT Bombay
• Lagrange introduced the stream function qi and the CI 223 I II /Slide S
corresponding velocity potential function
• Two dependent variables u and v are expressed in terms of one dependent variable
• At a given instant of time the stream function qi = tp(x,y)
STREAM FUNCTION (CONTD) CDEEP
IIT Bombay
CE 223
ovi ow _=u and = v • Property of a Lp function: cx
= const gives the equation of a streamline
LP exists for rotational and irrotational flows
V 2 v =0 For irrotational flow
The discharge between two streamlines w2 and 4J1
dip
VELOCITY POTENTIAL CDEEP
IIT Bombay
CI 223 L I I /Slide 1 0
• A velocity potential is introduced for irrotational flows
• The gradient of in any direction gives the velocity in that
direction: 30 30 ax ay
• 0 = constant represents an equipotential line
VELOCITY POTENTIAL (CONTD) CDEEP
IIT Bombay
• For an equipotential line dcp = 0
CE 223 L I I /Slide 1 1
a 0 a 0 dv u 610 = — dx + — dv=- u dx - v dy > =-
ax ay -
dx
• Similarly for a to = constant line dyi = 0 and dy = v
dx u
• Product of slopes of cl) and qi lines is (-1)
• cl) and iv lines are orthogonal
FLOWNET CDEEP
IIT Bombay
CE 223 L I I !Slide 12,
• A set of 1:1 and qi lines with spacing maintained equal
between cip, lines and qi lines is known as a flow net
• Flow net represents the solution of Laplace equation
\-7/*
= o
FLOWNET (CONTD)
• Methods of Solution :
r Graphical - free hand drawing
r Plotting equations for qi and cp lines
r Numerical solution of Laplace equation
r Conformal mapping
r Electrical and viscous flow analogy
CDEEP IIT Bombay
GE 223 IlL/Slide_13
• Velocity field is determined from continuity equation
and condition of irrotationality
• The equation of motion is not used
FLOWNET (CONTD) CDEEP
IIT Bombay
CE 223 L t i ;Slide 1 4
• Knowing the velocity field the pressure field
can be found based on Bernoulli's equation
• Superposition: Functions that individually satisfy
Laplace equation may be added together to describe a complex potential flow
• Inverse Method for getting ip and cD functions: Equations
are not directly solved
\ tra4 cs-tConcd-
CDEEP IIT Bombay
7 flif , 0
V zet?6 :a o
\71421 = 0 vrQeyia „ V"Er?,4-12)
a Le '
Sot eypos i 9/ c3 rt.
CE 223 Lit / Slide IS