ch2 fluid properties
TRANSCRIPT
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CE 351
Engineering Fluid Mechanics
CHAPTER 2Fluid Properties
Prof. Maed A!u"#reig
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$ntroduction
Field of Fluid Mechanics can !e di%ided into 3
!ranches&
Fluid 'tatics& (echanics of fluids at rest )ine(atics& deals *ith %elocities and
strea(lines *+o considering forces or energ,
Fluid -,na(ics& deals *ith the relations !et*een%elocities and accelerations and forces eerted
!, or upon fluids in (otion
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$ntro/con0t
Mechanics of fluids is etre(el, i(portant in (an,areas of engineering and science. Ea(ples are&
io(echanics lood flo* through arteries Flo* of cere!ral fluid
Meteorolog, and cean Engineering
Mo%e(ents of air currents and *ater currents Che(ical Engineering
-esign of che(ical processing euip(ent
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$ntro/con0t
Mechanical Engineering-esign of pu(ps4 tur!ines4 air"conditioning
euip(ent4 pollution"control euip(ent4 etc. Ci%il EngineeringTransport of ri%er sedi(ents
Pollution of air and *ater -esign of piping s,ste(sFlood control s,ste(s
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-i(ensions and nits
efore going into details of fluid
(echanics4 *e stress i(portance of units
$n .'4 t*o pri(ar, sets of units are used&1. '$ 6',ste(e $nternational7 units
2. English units
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nit Ta!le
8uantit, '$ nit English nit
9ength 697 Meter 6m) Foot 6ft 7
Mass 6(7 )ilogra( 6kg 7 'lug 6slug7 :lb*sec 2 /ft
Ti(e 6T7 'econd 6s7 'econd 6sec 7
Te(perature 6 7 Celcius 6oC 7 Farenheit 6oF 7
Force ;e*ton(N)=kg*m/s2
Pound 6l!7
θ
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-i(ensions and nits con0t
1 Newton < Force reuired to accelerate a
1 kg of (ass to 1 m/s2
1 slug < is the (ass that accelerates at 1
ft/s2 *hen acted upon !, a force of 1 lb
To re(e(!er units of a ;e*ton use F:(a
6;e*ton0s 2nd 9a*7 =F> : =(>=a>: kg*m/s2 = N
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More on -i(ensions
To re(e(!er units of a slug also use
F:(a :? ( : F + a
=(> : =F> + =a> : lb / (ft / sec 2 ) = lb*sec 2 / ft
1 lb is the force of gra%it, acting on 6or
*eight of 7 a platinu( standard *hose
(ass is @.535B23 kg
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eight and ;e*ton0s 9a* of Dra%itation
eightDra%itational attraction force !et*een t*o !odies
;e*ton0s 9a* of Dra%itation F : D (1(2+ r 2
D " uni%ersal constant of gra%itation
(14 (2 " (ass of !od, 1 and !od, 24 respecti%el, r " distance !et*een centers of the t*o (asses F " force of attraction
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eight
(2 " (ass of an o!ect on earth0s surface (1 " (ass of earth
r " distance !et*een center of t*o (asses
r 1 " radius of earth
r 2 " radius of (ass on earth0s surface
r 2 r 14 therefore r : r 1r 2 G r 1
Thus4 F : (2 6D (1 + r 27
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eight
eight 67 of o!ect 6*ith (ass (27 on surface of earth6*ith (ass (17 is defined as
: (2g I g :6D(1+r 27 gra%itational acceleration
g : B.J1 m/s2 in '$ units
g : 32.2 ft/sec 2 in English units
'ee !acK of front co%er of tet!ooK for con%ersion ta!les!et*een '$ and English units
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τ =
F
A s h e a r s t r e s s
x
( )
L 'hear stress and pressure
p F
A n o r m a l s t r e s s p r e s s u r e
z= ( ( ) )
L 'hear stress and pressure at a point
τ =
→
F
A
x
Al i m 0
p F
A
z
A
=
→
l i m 0
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[ ]
[ ] ( )
F
A
N
m P a P a s c a l i n S I u n i t s= =2
L nits of stress 6shear stress and pressure7
[ ]
[ ]
( ) F
A
l b
i n
p s i p o u n d s p e r s q u a r e i n c h i n E n g l i s h u n i t s= =2
[ ]
[ ] ( )
F
A
l b
f t p o u n d s p e r s q u a r e f o o t E n g l i s h u n i t s= =2
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Properties of Fluids Con0t
Fluids are either liuids or gases
9iuid& A state of (atter in *hich the (olecules
are relati%el, free to change their positions *ithrespect to each other !ut restricted !, cohesi%e
forces so as to (aintain a relati%el, fied %olu(e
Das& a state of (atter in *hich the (olecules
are practicall, unrestricted !, cohesi%e forces. A
gas has neither definite shape nor %olu(e.
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More on properties of fluids
Fluids considered in this course (o%e
under the action of a shear stress4 no
(atter ho* s(all that shear stress (a, !e6unliKe solids7
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-efinition of a Fluid
hen a shear stress is applied& Fluids continuousl, defor(
'olids defor( or !end
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Continuu( %ie* of Fluids
Con%enient to assu(e fluids are continuousl, distri!uted
throughout the region of interest. That is4 the fluid is
treated as a continuu(
This continuu( (odel allo*s us to not ha%e to deal *ith
(olecular interactions directl,. e *ill account for such
interactions indirectl, %ia %iscosit,
A good *a, to deter(ine if the continuu( (odel is
accepta!le is to co(pare a characteristic length of theflo* region *ith the (ean free path of (olecules4
$f 4 continuu( (odel is %alid
( ) Lλ
L < < λ
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-ensit, and specific *eight
-ensit, 6(ass per unit %olu(e7& ρ = m
V
[ ]
[ ]
[ ] ( ) ρ = =m
V
k g
m i n S I u n i t s3nits of densit,&
'pecific *eight 6*eight per unit %olu(e7&
[ ] [ ] [ ] ( )γ ρ = = = g k g
m
m
s
N
mi n S I u n i t s3 2 3
nits of specific *eight&
γ ρ = g
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'pecific Dra%it, of 9iuid 6S7
'ee appendi A of tet!ooK for specific
gra%ities of %arious liuids *ith respect to
*ater at @ oF
ater
liquid
ater
liquid
ater
liquid
g
g S
γ
γ
ρ
ρ
ρ
ρ ===
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Niscosit, 6 7
Niscosit, can !e thought as the internal sticKiness of a fluid
Representati%e of internal friction in fluids
$nternal friction forces in flo*ing fluids result fro( cohesionand (o(entu( interchange !et*een (olecules.
Niscosit, of a fluid depends on te(perature& $n liuids4 %iscosit, decreases *ith increasing te(perature 6i.e.
cohesion decreases *ith increasing te(perature7
$n gases4 %iscosit, increases *ith increasing te(perature 6i.e.
(olecular interchange !et*een la,ers increases *ith te(perature
setting up strong internal shear7
µ
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More on Niscosit,
Niscosit, is i(portant4 for ea(ple4 in deter(ining a(ount of fluids that can !e
transported in a pipeline during a specificperiod of ti(e
deter(ining energ, losses associated *ith
transport of fluids in ducts4 channels and
pipes
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;o slip condition
ecause of %iscosit,4 at !oundaries 6*alls7
particles of fluid adhere to the *alls4 and
so the fluid %elocit, is Oero relati%e to the*all
Niscosit, and associated shear stress (a,
!e eplained %ia the follo*ing& flo*!et*een no"slip parallel plates.
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'o(e 'i(ple Flo*s
Flo* !et*een a fied and a (o%ingplate
Fluid in contact *ith the plate has the sa(e
%elocit, as the plate
u : x "direction co(ponent of %elocit,
u=V Mo%ing plate
Fied plate
y
x
V
u=@
B ! "
V !u =)( Fluid
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'o(e 'i(ple Flo*s
Flo* through a long4 straight pipe
Fluid in contact *ith the pipe *all has the
sa(e %elocit, as the *all
u : x "direction co(ponent of %elocit,
x
!
−=2
1)(
#
r V r u
V Fluid
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The %elocit, induced !, (o%ing top plate can !e sKetched as follo*s&
!
u !( )
$
%
u !%
$ !( ) =
The %elocit, induced !, top plate is epressed as follo*s&
u !( )= =0 0
u ! $ % ( )= =
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For a large class of fluids4 e(piricall,4 F A %
$ ∝
More specificall,4 F A % $
= µ ; µ i s c o e f f i c i e n t o f & i s i t !c o s
'hear stress induced !, is F τ µ = = F
A
%
$
Fro( pre%ious slide4 note thatd u
d !
%
$ =
Thus4 shear stress is τ µ = d ud !
$n general *e (a, use pre%ious epression to find shear stress at a point
inside a (o%ing fluid. ;ote that if fluid is at rest this stress is Oero !ecause
d u
d ! = 0
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;e*ton0s euation of %iscosit,
τ µ = d u
d !
µ " %iscosit, 6coeff. of %iscosit,7
Fied no"slip plate
u ! & e l o c i t ! p r o f i l e( ) ( )
'hear stress due to %iscosit, at a point&
fluid surface
e.g.& *ind"dri%en flo* in ocean
ν µ ρ =
" Kine(atic%iscosit,
!
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As engineers4 ;e*ton0s 9a* of Niscosit, is %er, useful to us as *e can use it to
e%aluate the shear stress 6and ulti(atel, the shear force7 eerted !, a (o%ing
fluid onto the fluid0s !oundaries.
τ µ a t b o u n d a r !d u
d !a t b o u n d a r !
=
;ote is direction nor(al to the !oundar, !
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Flo* !et*een 2 plates
u=V Mo%ing plate
Fied plate
y
x
V
u=@
B ! "V !u =)( Fluid Force acting; the plate
21
21
222111
τ τ
τ τ
=
=
===
A A
F A A F
2211 τ µ µ τ === d!du
d!
du
Thus4 slope of %elocit,
profile is constant and
%elocit, profile is a st. line
Force is sa(e on top
and !otto(
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Flo* !et*een 2 plates
u=V Mo%ing plate
Fied plate
y
x
V
u=@
B ! "V !u =)(
"
V
d!
du
µ µ τ ==
'hear stress an,*here
!et*een plates
τ
τ
'hear on fluid
m "
smV
' SAE m s N o
02.0
/3
)38@30(/1.0 2
=
=⋅= µ
2
2
/15
)02.0
/3)(/1.0(
m N
m
smm s N
=
⋅=τ
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Ea(ple& ournal earing
Di%en Rotation rate4 ω : 15@@ rp(
d : c(
l : @ c(
" : .@2 c(
S#oil : @.JJ
νoil : @.@@3 (2+s
Find& Torue and Po*erreuired to turn the !earing
at the indicated speed.
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Ea(ple& cont.
Assu(e& 9inear %elocit, profile in oil fil(
2/1242/)0002.0(
)2/06.0(1500*60
2
)003.0*998*88.0(
2/)(
)2/( StressShear
mkN
d (
d
d!
dV
=
=
−==
π
ω µ µ τ
m N
d l
d )
⋅==
=
2812
06.0)4.0*
2
06.0*000124*2(
2
)
2
2(!or"#e
π
πτ
k* sm N ) P 1.44/100441.15$*281%o&er =⋅=== ω
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Nisco(eter
Coefficient of %iscosit, can !e (easured e(piricall, using a %isco(eter µ
Ea(ple& Flo* !et*een t*o concentric c,linders 6%isco(eter7 of length
Mo%ing fluid
Fied outer
c,linder
Rotating inner
c,linder
ω +
r
#
h
x
z
!
r " radial coordinate
,
L
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$nner c,linder is acted upon !, a torue4 4 causing it to
rotate a!out point at a constant angular %elocit, and
causing fluid to flo*. Find an epression for
+ + k = ω ,
ecause is constant4 is !alanced !, a resisti%e torue
eerted !,
the (o%ing fluid onto inner c,linder
ω + + k =
+ + k r e s r e s= −( )
The resisti%e torue co(es fro( the resisti%e stress eerted !, the
(o%ing fluid onto the inner c,linder. This stress on the inner c,linder leads
to an o%erall resisti%e force 4 *hich induces the resisti%e torue a!out
point
x
!
z
,
+ + r e s=
+
τ r e s
⇒+
F r e s
τ r e s
# ⇒+ + r e s
F
r e s
+
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+ + F #r e s r e s= =
F A # Lr e s r e s r e s= =τ τ π ( )2 6;eglecting ends of c,linder7
Ho* do *e get Q This is the stress eerted !, fluid onto inner
c,linder4 thus
τ r e s
τ µ r e s
a t i n n e r c ! l i n d e r r #
d u
d r =
=( )
$f 6gap !et*een c,linders7 is s(all4 thenh
r
u r ( )
# ω
r # h= +r #=
d u
d r
#
ha t i n n e r c ! l i n d e r r #( )=
= ω
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Thus4 τ µ ω
r e s #
h=
+ + F #r e s r e s= =
+ + A # # L #r e s r e s r e s= = =τ τ π ( )2
=
µ ω
π #
h # L #( )2
+ # Lh
=3
2 µ ω π
Di%en pre%ious result (a, !e used to find of
fluid4 thus concentric c,linders (a, !e used as a %isco(eter
+ # L h ω µ
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Ea(ple& Rotating -isK
Assu(e linear %elocit, profile& dV/dy :V/y :ω /y
Find shear stress
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'urface Tension
elo* surface4 forces act euall,
in all directions
At surface4 so(e forces are
(issing4 pulls (olecules do*n andtogether4 liKe (e(!rane eerting
tension on the suf$ce
$f interface is cur%ed4 higher
pressure *ill eist on conca%e side
Pressure increase is !alanced !,surface tension4 σ
σ : @.@3 ;+( 6S 2@oC7
*ater
air
;o net force
;et force
in*ard
$nterface
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'urface tensionL Consider inserting a fine tu!e into a !ucKet of *ater&
h
σ σ
Meniscus
x
!
σ " 'urface tension %ector 6acts unifor(l, along contact peri(eter !et*een liuid and tu!e7
Adhesion of *ater (olecules to the tu!e do(inates o%er cohesion !et*een
*ater (olecules gi%ing rise to and causing fluid to rise *ithin tu!eσ
θ θ
r " radius of tu!e
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h
σ σ θ θ
*
x
! σ σ θ θ = +[ s i ' ( ) c o s ( ) ]i -
* * -= −( ) 6*eight %ector of *ater7
Euili!riu( in y%diection ,ields& σ θ π c o s ( ) ( ) ( ) 2 0r - * - -+ − =
Thus σ π θ = * r 2 c o s
*ith * r h a t e r = γ π 2
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Co(pressi!ilit,
L All fluids co(press if pressure increases resulting in an
increase in densit,
L Co(pressi!ilit, is the change in %olu(e due to a
change in pressure
L A good (easure of co(pressi!ilit, is the !ulK (odulus
6$t is in%ersel, proportional to co(pressi!ilit,7
E d p
d υ υ
υ = −
υ ρ = 1
( ) s p e c i f i c & o l u m e
p i s p r e s s u r e
ρ ρ // ∆∆=
∆∆−= p
V V p E&
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Co(pressi!ilit,
L Fro( a!o%e epression4 increasing pressure !, 1@@@ &si *ill co(press
the *ater !, onl, 1+32@ [email protected] of itsoriginal %olu(e
E p s iυ = 3 2 0 0 0 0
L Thus4 *ater (a, !e treated as inco(pressi!le 6densit, is constant7 ( ) ρ
L $n realit,4 no fluid is inco(pressi!le4 !ut this is a good approi(ation for certain fluids
L For *ater ' : 2.2 DPa4
1 MPa pressure change : @.@5 %olu(e change
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Napor pressure of liuidsL All liuids tend to e%aporate *hen placed in a closed container
L NaporiOation *ill ter(inate *hen euili!riu( is reached !et*eenthe liuid and gaseous states of the su!stance in the container
i.e. U of (olecules escaping liuid surface : U of inco(ing (olecules
L nder this euili!riu( *e call the call %apor pressure the saturation pressure
L At an, gi%en te(perature4 if pressure on liuid surface falls !elo* the the saturation pressure4 rapid e%aporation occurs 6i.e. !oiling7
L For a gi%en te(perature4 the saturation pressure is the !oiling pressure
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Napor Pressure
Pressure at *hich a liuid*ill !oil for gi%en te(p.
Napor pressure increases
*ith te(perature $ncreasing te(perature of
*ater at sea le%el to 212 oF4increases the %aporpressure to 1. psia and!oiling occurs
oiling can occur !elo* 212 oFif *e lo*er the pressure in the*ater to the %apor pressure ofthat te(perature
Vapor Press. vs. Temp.
0
20
40
60
80
100
120
0 10 20 30 40 50 60 0 80 !0 100
Temperature "o#$
V a p r o
P r e s s u r e " % P a $
L At 5@ oF4 the %aporpressure is @.1J psia
L $f ,ou reduce thepressure in *ater at thiste(perature4 !oiling *illoccur 6ca%itation7
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Ta&le '.2PHV'$CA9 PRPERT$E' F DA'E' AT 'TA;-AR-
ATM'PHER$C PRE''RE A;- 15WC 65BWF7
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Ea(ple
Di%en& ;atural gas
Ti(e 1& 1:1@oC4 &1:1@@ KPa
Ti(e 2& 2:1@oC4 &2:2@@ KPa
Find& Ratio of (ass at ti(e 2 to that at ti(e 1
$deal gas la* 6 & is a!solute pressure7
V #+
pV ) == ρ
2
1
2
1
2
1
p
p
V
#+
p
V #+
p
)
) ==
5.1200
300
1
2 ==kPa
kPa
)
)
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Ea(ple
Esti(ate the (ass of 1 (i3 of air
in slugs and Kgs
Assu(e ρ $i : @.@@23 slugs+ft34
the %alue at sea le%el for standard
conditions
kg x )
slugskg slugs x )
slugs x )
V ) air
9
8
8
3
1009.5
/59.14*1049.3
1049.3
)2805(*0023$.0
=
=
=
== ρ
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Ea(ple
(iven) Pressure of 2 MPa is
applied to a (ass of *ater that
initiall, filled 1@@@"c(3 %olu(e.
*ind) Nolu(e after the
pressure is applied.
+olution) E : 2.21@B Pa
"Ta!le A.57
3
3
3
9
6
01.999
909.01000
909.0
1000102.2
102
/
cmV
V V V
cm
cm Pa x
Pa x
V E
pV
V V
p E
final
final
&
&
=
−=∆+=
−=
−=
∆−=∆
∆∆−=
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Capillar, Rise
(iven) ater S 2@oC4d : 1. ((
*ind) Height of *ater +olution) 'u( forces in
%ertical
Assu(e θ s(all4 cosθ 1
0)4
)((cos
0
2
=∆−=−
d hd
* F z π
γ θ σπ
σ
mmh
x
d h
6.18
106.1*9$90
0$3.0*4
4
3
=∆
=
=∆
−
γ
σ
σ F
W
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Ea(ple 62.517
*ind) Capillar, rise !et*een t*o
%ertical glass plates 1 (( apart.
σ : .31@"2 ;+(
l is into the page
+olution)
t
σ σ
θ
mmh
mh
x
t h
hlt l
F &ertical
9.14
0149.0
9810*001.0103.$*2
2
02
0
2
==
=
=
=−=∑
−
γ
σ
γ σ
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Ea(ples of 'urface Tension
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Ea(ple
*ind) The for(ula for the gage
pressure *ithin a sperical
droplet of *aterQ
+olution) 'urface tensionforce is reisited !, the force
due to pressure on the cut
section of the drop
r p
r r pσ
σ π π 2
2)( 2
=
=
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Ea(ple 62.J7 (iven) 'perical !u!!le4
inside radius 4 fil( thicKness
t 4 and surface tension σ .
*ind) For(ula for pressure
in the !u!!le relati%e to that
outside.
+olution)
Pa p
x p
r
p
r r p
F
0.$3
004.0
103.$*4
4
0)2(2
0
2
2
=∆
=∆
=∆
=−∆
=∑
−
σ
σ π π
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ug Pro!le(
σ
Cross"section
of !ug leg
σ
F