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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

    [ ]

    [ ]

    [ ]   ( ) ρ    = =m

    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

     x 

    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

     x 

    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

     x 

    u=@

    B   ! "V  !u   =)(

     "

    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!

    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    + 

     #

    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

    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

     #+ 

     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 

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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) 

    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

     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