forced covection - thermo lab report

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  • 8/9/2019 Forced Covection - Thermo Lab Report

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    ohammed Zaid Shaikh –00114083This document contains a report on

    forced convection around a

    cylindrical copper rod of diameter

    001!" m

    #orced

    $ovectionhermo la% &eport

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    FORCED CONVECTION – THERMO LAB REPORT

    INTRODUCTION

     This report covers the heat transfer rate from a cylindrical copper rod to the

    surroundin' air movin' at a certain ()ed velocity in an isolated system *esides

    sho+in' ho+ the heat transfer rate is a,ected %y varyin' the velocity of air in

    the isolated system this e)perimental la% report also sho+s the calculations for

    &eynolds num%er- .usselt num%er- as +ell as the (lm heat transfer coe/cient

    Moreover- it covers %rief discussion on the comparison of the e)perimental

    values of 2 and n2 from the %elo+ euation +ith that of their literature values

     Nu= K ℜn

    n this e)periment the heat transfer rate associated +ith the cross 5o+ of air

    across a cylindrical copper rod at various velocities has %een investi'ated The

    aim of the e)periment is to determine the heat transfer characteristics of a

    cylinder under cross 5o+ forced convection conditions +hen the cylinder is

    isolated The follo+in' euation is used to plot the 'raph and hence the slope of

    the 'raph +as used to calculate the estimated heat transfer coefficient 6

    ( ) ( )a p

    a   T T t C m

     AT T    −+−=−

    0lnln

      α 

     This e)periment also helps in understandin' the comple)ities in heat transferrin'

    durin' the cross 5o+ across a cylindrical copper rod 7n chan'in' the velocity of

    the +ind- the &eynolds num%er of the 5o+ chan'es +hich then a,ects the heat

    transfer Fig. a9 %elo+ sho+s a 'raphical representation on ho+ increasin' the

    &eynolds num%er chan'es the nature of the 5o+

    :ractical and &eal ;ife

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    report can hence %e used as reference +hen desi'nin' a car radiator +ith copper

    metal for am%ient temperature of !3>$

    !

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    Fig. a

    3

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    PROCEDURE AND APPARATUS

     The follo+in' procedures +ere undertaken for this e)periment=

    19 The apparatus +as checked %y the la% supervisor

    !9 The air duct +as s+itched on

    39 The air speed +as set to 3 m?s usin' the kno%

    49 The copper cylindrical rod +as heated up to @A>$ in an electric heated

    "9 The copper rod +as then placed inside the air duct throu'h one of the hole

    B9 The temperature drop +as noted after every " seconds usin' a thermometer

    and stop+atch

    A9 Steps 3CB +ere repeated to take readin's at di,erent +ind speed

     The follo+in' apparatus +ere used for the e)periment

    • $ross 5o+ heat e)chan'er Fig. B9

    • Dlectric heater

    • $opper cylindrical rod

    • Stop +atch

    RESULTS

    4

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    Eiven Fata=

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    1!0 B4B "33 "1! 4@1 4AB

    $alculated Fata u=3 m/ s

    Time(s)

    Temp T @

    !"m#s($C

    )

    Amie*+

    Temp Ta

    ($C)

    T,Ta ($C) L*(T,Ta)

    0 @A0 !3 A4 43040B"" @A0 !3 A4 43040B"10 @!A !3 B@A 4!44!1" @!A !3 B@A 4!44!!0 88B !3 B"B 4183"AB!" 88B !3 B"B 4183"AB30 8A1 !3 B41 41B04443" 8A1 !3 B!1 41!8A4B40 8!0 !3 "@0 40AA"3A4" 8!0 !3 "@0 40AA"3A"0 A@1 !3 "B1 40!A13B"" A@1 !3 "B1 40!A13BB0 AA1 !3 "41 3@@0834B" AA1 !3 "41 3@@0834A0 A4! !3 "1! 3@3"A4A" A4! !3 "1! 3@3"A480 A!4 !3 4@4 38@@@"8" A!4 !3 4@4 38@@@"@0 A04 !3 4A4 38"8B!!

    @" A04 !3 4A4 38"8B!!100 B83 !3 4"3 381330A10" B83 !3 4"3 381330A110 BB4 !3 434 3AA04"@11" BB4 !3 434 3AA04"@1!0 B4B !3 41B 3A!81

    $alculations=

    @u=3 m /s

    u=3 m / s

    v=  u

    0.9=

      3

    0.9=3.33

    µ=18.3808 Pa . s

     ρa

    =1.17656 kg/m3

    B

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    d=0.0125 m

    b=0.125 m

    h=0.125 m

    k =0.0259 W /(m . K )

     Heat transfer ceff!c!ent " # =−$%pe f graph 1 & m & C   p

     A

    # 3=−−0.0048 &0.21 &380

    0.00404

    # 3=94.8 W /(m2

    . K )

    Similarly- @u=5,7,9,∧11 heat transfer coe/cient is calculated

    # 5=150.12 W /(m2

    . K )

    # 7=167.9 W /(m2

    . K )

    # 9=169.87 W /(m2

    . K )

    # 11=185.67 W /(m2

    . K )

     Nusse%t number " Nu=# d

     Nu3=

    94.8& 0.0125

    0.0259=46

    Similarly- @u=5,7,9,∧11  .usselt num%er is calculated

     Nu5=73

     Nu7=82

    A

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     Nu9=83

     Nu11=90

    ℜ= ρ a v d

    µ

    ℜ3=1.17656 &3.333 & 0.0125

    18.3808=2667

    Similarly- @u=5,7,9,∧11  &eynolds num%er is calculated

    ℜ5=4445

    ℜ7=6315

    ℜ9=8119

    ℜ11=9924

    :randlt .um%er-  Pr=C 

     p& '

    k   

     Pr=0.27

    Eraphical $alculations=

    8

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    0 !0 40 B0 80 100 1!0 1403

    3"

    4

    4"

    "

    -() ! , / 0 1."

    Ln (T-Ta) vs t 

    ln ITCTaJ

    ;inear ln ITCTaJ9

    Time

    2* ()T,Ta

    3RAPH 4

    0 !0 40 B0 80 100 1!0 140

    0

    10

    !0

    30

    40

    "0

    B0

    A0

    80

    -() ! &".% ep( / )

    (T-Ta) vs t 

    ITCTaJ

    D)ponential ITCTaJ9

    Time

    T,Ta

    3RAPH 45

    @

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    !000 4000 B000 8000 10000 1!000 14000

    0

    10

    !0

    30

    40

    "0

    B0

    A0

    80

    @0

    100

    -() ! .% 6/.1%

    Nu vs Re

      :o+er 9

    Re7*829s *:me;

    N:sse2+ *:me;

    3RAPH 4"

    Kalues from Eraphical Duations=

    #rom Eraph L1= Slope C 00048

    #rom Eraph L3=  Nu= K ℜn

    Ghere-

       K =1.5066 - n=0.4462

    DISCUSSION

     The $orrelation literature value for ( k (   and   ( n 2 for the euation  Nu= K ℜn

     

    +ere found as follo+s=

     K =1.15

    n=0.5

    Drror

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     )rrr = )*per!menta% va%ue− +!teratureva%ue

     +!terature va%ue  &100

     )rrr fr K =1.5066−1.15

    1.15

    &100=31

     )rrr fr n=0.4462−0.5

    0.5& 100=−10.7

     

    Nsin' a%ove values of  K   and   n - +e (nd  Nu  theoretical

    Kelocity u   m /s 9 &eynolds .um%er   ℜ¿ .usselt .um%er   Nu 9

    3   2667   59

    5 4445 77

    7   6315 91

    9 8119 103

    11 9924 114

    :lottin' the 'raph for literature value of

     Nu

     vs

    ℜ +e 'et-

    11

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    !000 4000 B000 8000 10000 1!0000

    !0

    40

    B0

    80

    100

    1!0

    f)9 11B )O0"

    Nu vs Re

    .u

    :o+er .u 9

    Re7*829 *:me;

    N:sse2+ *:me;

    3RAPH 41

    $omparin' the 'raph L3 and 'raph L4=

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    !000 4000 B000 8000 100001!000

    0

    !0

    40

    B0

    80

    100

    1!0

    f)9 0@8 )O0"

    f)9 11B )O0"

    .u literature

    :o+er .u literature9

    .u

    :o+er .u9

    Re7*829s *:me;

    N:sse2+ *:me;

    3RAPH 4%

    :ossi%le errors durin' the e)periment=

    • Karyin' am%ient temperature

    • Slo+ di'ital thermocouple

    •  Timin' calculation +hile usin' the stop+atch

    • Karyin' +ind speed from the air duct

    CONCLUSION

     The e)perimental results +ere almost as e)pected Drror P for the calculations

    +as less This e)periment sho+s ho+ the heat transfer rate chan'es under the

    circumstances of forced convection n conclusion to the e)perimental result the

    follo+in' points can %e noted=

    1 7n increasin' the +ind speed the copper rod cools faster! The thermal coe/cient increases +ith the increase in &eynolds num%er

    3 $opper is a 'ood conductor of heat4 $onvection is an important part of real life applications and can cause

    serious en'ineerin' pro%lems if not dealt +ith properly

    REFERENCE

    1 ;ienhard- QH- K R ;ienhard- QH K- < Heat Transfer Te)t%ook- 4th Dd-

    $am%rid'e- M