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    Week9

    4.7MomentDistributionMethodforMultiRedundantBeams

    Thissectiondealswithcontinuousbeamsandproppedcantilevers.AnAmericanengineer,Professor

    HardyCross,developedaverysimple,elegantandpracticalmethodofanalysisforsuchstructurescalledMomentDistribution.Thistechniqueisoneofdevelopingsuccessiveapproximationsandis

    basedonseveralbasicconceptsofstructuralbehaviour.

    4.7.1Bending(Rotational)Stiffness

    Afundamentalrelationshipwhichexistsintheelasticbehaviourofstructuresandstructural

    elementsisthatbetweenanappliedforcesystemandthedisplacementswhichareinducedbythat

    system,i.e.

    Force=StiffnessxDisplacement

    P=k

    Where

    Pistheappliedforce,

    kisthestiffness,

    isthedisplacement.

    Adefinitionofstiffnesscanbederivedfromthisequationbyrearrangingitsuchthat:

    k=P/

    when =1.0 (i.e.unitdisplacement)thestiffnessis:theforcenecessarytomaintainaUNIT

    displacement,allotherdisplacementsbeingequaltozero.

    Thedisplacementcanbeasheardisplacement,anaxialdisplacement,abending(rotational)

    displacementoratorsionaldisplacement,eachinturnproducingtheshear,bendingortorsional

    stiffness.

    Whenconsideringbeamelementsincontinuousstructuresusingthemomentdistributionmethod

    ofanalysis,thebendingstiffnessistheprincipalcharacteristicwhichinfluencesbehaviour.

    ConsiderthebeamelementABshowninFigure4.67whichissubjecttoaUNITrotationatendAand

    isfixedatendBasindicated.

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    Figure4.67

    Theforce(MA)necessarytomaintainthisdisplacementcanbeshowntobeequalto(4EI)/L.From

    thedefinitionofstiffnessgivenpreviously,thebendingstiffnessofthebeamisequalto(Force/1.0),

    thereforek=(4EI)/L.Thisisknownastheabsolutebendingstiffnessoftheelement.Sincemost

    elementsincontinuousstructuresaremadefromthesamematerial,thevalueofYoung'sModulus

    (E)isconstantthroughoutand4Einthestiffnesstermisalsoaconstant.Thisconstantisnormally

    ignored,togivek=I/Lwhichisknownastherelativebendingstiffnessoftheelement.ItisthisvalueofstiffnesswhichisnormallyusedinthemethodofMomentDistribution.

    ItisevidentfromFigure4.67thatwhenthebeamelementdeformsduetotheappliedrotationat

    endA,anadditionalmoment(MB)isalsotransferredbytheelementtotheremoteendifithaszero

    slope(i.e,isfixed).ThemomentMBisknownasthecarryovermoment.

    4.7.2 CarryOverMoment

    Usingthe

    same

    analysis

    asthat

    todetermine

    MA,

    itcan

    be

    shown

    that

    MB

    =(2EI)/L,

    i.e.

    (1/2

    xMA),

    It

    canthereforebestatedthatifamomentisappliedtooneendofabeamthenamomentofthe

    samesenseandequaltohalfofitsvaluewillbetransferredtotheremoteendprovidedthatitis

    fixed.

    Iftheremoteendispinned,thenthebeamislessstiffandthereisnocarryovermoment.

    4.7.3 PinnedEnd

    ConsiderthebeamshowninFigure4.68inwhichaunitrotationisimposedatendAasbeforebut

    theremoteendBispinned.

    Figure4.68

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    Theforce(MA)necessarytomaintainthisdisplacementcanbeshown(e.g.usingMcCaulay's

    Method)tobeequalto (3EI)/L,whichrepresentsthereducedabsolutestiffnessofapinended

    beam.Itcanthereforebestatedthatthestiffnessofapinendedbeamisequalto4

    3xthestiffness

    ofafixedendbeam.Inadditionitcanbeshownthatthereisnocarryovermomenttotheremote

    end.ThesetwocasesaresummarisedinFigure4.69.

    Figure4.69

    4.7.4FreeandFixedBending;Moments

    WhenabeamisfreetorotateatbothendsasshowninFigures4.70(a)and(b)suchthatnobending

    momentcandevelopatthesupports,thenthebendingmomentdiagramresultingfromtheapplied

    loadsonthebeamisknownastheFreeBendingMomentDiagram.

    Figure4.70 FreeBendingMomentDiagrams

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    Whenabeamisfixedattheends(encastre)suchthatitcannotrotate,i.e.zeroslopeatthe

    supports,asshowninFigure4.71,thenbendingmomentsareinducedatthesupportsandarecalled

    FixedEndMoments.Thebendingmomentdiagramassociatedonlywiththefixedendmomentsis

    calledtheFixedBendingMomentDiagram.

    Figure4.71 FixedBendingMomentDiagram

    Usingtheprincipleofsuperposition,thisbeamcanbeconsideredintwopartsinordertoevaluate

    thesupportreactionsandtheFinalbendingmomentdiagram:

    i. The,fixedreactions(momentsandforces)atthesupportswithoutappliedloadonthebeam

    Figure4.72

    ii. Thefreereactionsatthesupportsandthebendingmomentsthroughoutthelengthdueto

    theappliedload,assumingthesupportstobepinned

    Figure4.73

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    Combining(i)+(ii)givesthefinalbendingmomentdiagramasshowninFigure4.74:

    Figure4.74

    Note:

    ThevaluesofMAandMBforthemostcommonlyappliedloadcasesaregivenAppendix2.Theseare

    standardFixedEndMomentsrelatingtosinglespanencastrebeamsandareusedextensivelyin

    structuralanalysis.

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    4.7.5 Example4.19:SinglespanEncastreBeam

    Determinethesupportreactionsanddrawthebendingmomentdiagramfortheencastrebeam

    loadedasshowninFigure4.75.

    Figure4.75

    Solution:

    Considerthebeamintwoparts.

    (i)FixedSupportReactions

    ThevaluesofthefixedendmomentsaregiveninAppendix2.

    Considertherotationalequilibriumofthebeam:

    Considertheverticalequilibriumofthebeam:

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    (ii)Considertherotationalequilibriumofthebeam:

    Considertheverticalequilibriumofthebeam:

    BendingMomentunderthepointload=(+13.33x2.0)=+26.67kNm

    (Thisinducestensioninthebottomofthebeam)

    Thefinalverticalsupportreactionsaregivenby(i)+(ii):

    Checktheverticalequilibrium:

    Totalverticalforce=+ 14.81+5.19=?

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    M=?

    Fixedbendingmomentdiagram

    Freebendingmomentdiagram

    Finalbendingmomentdiagram

    Figure4.76

    Notethesimilaritybetweentheshapeofthebendingmomentdiagramandthefinaldeflected

    shapeasshowninFigure4.77.

    Figure4.77Deflectedshapeindicatingtensionzonesandthesimilaritytotheshapeofthebending

    momentdiagram.

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    4.7.6ProppedCantilevers

    Thefixedendmomentforproppedcantilevers(i.e.oneendfixedandtheotherendsimply

    supported)canbederivedfromthestandardvaluesgivenforencastrebeamsasfollows.

    ConsidertheproppedcantilevershowninFigure4.78,whichsupportsauniformlydistributedloadasindicated.

    Figure4.78

    Thestructurecanbeconsideredtobethesuperpositionofanencastrebeamwiththeadditionofan

    equalandoppositemomenttoMBappliedatBtoensurethatthefinalmomentatthissupportis

    equaltozero,asindicatedinFigure4.79.

    Figure4.79.

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    4.7.7Example4.20:ProppedCantilever

    Determinethesupportreactionsanddrawthebendingmomentdiagramfortheproppedcontilever

    showninFigure4.80.

    Figure4.80.

    Solution

    FixedEndmomentforProppedCantilever:

    Considerthebeamfixedatbothsupports.

    ThevaluesofthefixedendmomentsforencastrebeamsaregiveninAppendix2.

    Themoment MBmustbecancelledoutbyapplyinganequalandoppositemomentatBwhichin

    turnproducesacarryovermomentequalto (0.5xMB)atsupportA.

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    Considertherotationalequilibriumofthebeam:

    Considertheverticalequilibriumofthebeam:

    Considertherotationalequilibriumofthebeam:

    Considertheverticalequilibriumofthebeam:

    Thefinalverticalsupportreactionsaregivenby(i)+(ii):

    Checkthe

    vertical

    equilibrium:

    Total

    vertical

    force

    =+50.0

    +30.0

    =+80

    kN

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    Figure4.81

    Notethesimilaritybetweentheshapeofthebendingmomentdiagramandthefinaldeflected

    shapeasshowninFigure4.82.

    Figure4.82

    Deflectedshapeindicatingtensionzonesandthesimilaritytotheshapeofthebendingmoment

    diagram

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    Thepositionofthemaximumbendingmomentcanbedeterminedbyfindingthepointofzeroshear

    forceasshowninFigure4.83.

    Figure4.83

    4.7.8DistributionFactors

    Considerauniformtwospancontinuousbeam,asshowninFigure4.84.

    Figure4.84

    IfanexternalmomentMisappliedtothisstructureatsupportBitwillproducearotationofthe

    beamatthesupport;partofthismomentisabsorbedbyeachofthetwospansBAandBC,as

    indicatedinFigure4.85.

    Figure4.85

    Theproportionofeachmomentinducedineachspanisdirectlyproportionaltotherelative

    stiffnesses,e.g.

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    Totalstiffnessofthebeamatthesupport

    ThemomentabsorbedbybeamBA

    ThemomentabsorbedbybeamBC

    Theratio isknownastheDistributionFactorforthememberatthejointwherethemomentisapplied.

    AsindicatedinSection 4.7.2,whenamoment(M)isappliedtooneendofabeaminwhichthe

    otherendisfixed,acarryovermomentequalto50%ofMisinducedattheremotefixedendand

    consequentlymomentsequalto1/2M1and1/2M2,willdevelopatsupportsAandCrespectively,as

    showninFigure4.86.

    Figure4.86

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    4.7.9 ApplicationoftheMethod

    AlloftheconceptsoutlinedinSections 4.7.1to4.7.8areusedwhenanalysingindeterminate

    structuresusingthemethodofmomentdistribution.Considerthetwoseparatebeamspans

    indicatedinFigure4.87.

    Figure4.87

    SincethebeamsarenotconnectedatthesupportBtheybehaveindependentlyassimplysupported

    beamswithseparatereactionsandbendingmomentdiagrams,asshowninFigure4.88.

    Figure4.88

    WhenthebeamsarecontinuousoversupportBasshowninFigure4.89(a),acontinuitymoment

    developsforthecontinuousstructureasshowninFigures4.89(b)and(c).Notethesimilarityofthe

    bendingmomentdiagramformemberABtotheproppedcantileverinFigure4.81.Bothmembers

    ABandBDaresimilartoproppedcantileversinthisstructure.

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    Figure4.89

    Momentdistributionenablestheevaluationofthecontinuitymoments.Themethodisideallysuited

    totabularrepresentationandisillustratedinExample4.21.

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    4.7.10 Example4.21:ThreespanContinuousBeam

    Anonuniform,threespanbeamABCDEFisfixedatsupportAandpinnedatsupportF,asillustrated

    inFigure4.90.Determinethesupportreactionsandsketchthebendingmomentdiagramforthe

    appliedloadingindicated.

    Figure4.90

    Solution:

    Step1

    Thefirststepistoassumethatallsupportsarefixedagainstrotationandevaluatethe'fixedend

    moments'.

    ThevaluesofthefixedendmomentsforencastrebeamsaregiveninAppendix2.

    SpanAC

    MAC=?

    MCA=?

    SpanCD

    MCD=?

    MDC=?

    SpanDF*

    MDF=?

    MFD=?

    *SincesupportFispinned,thefixedendmomentsare(MDF 0.5MFD)atDandzeroatF(seeFigure

    4.79):(MDF 0.5MFD)=[ 46.89 (0.5x46.89)]= 70.34kNm.

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    Step2

    Thesecondstepistoevaluatethememberandtotalstiffnessateachinternaljoint/supportand

    determinethedistributionfactorsateachsupport.Notethattheappliedforcesystemisnot

    requiredtodothis.

    SupportC

    SupportD

    Stiffness of DC= kDC= ?

    ktotal= (? + 0.225) I= 0.475 I

    Stiffness of DF= kDF*=

    4

    3(1.5 I / 5.0)= 0.225 I

    *Note: The remote end F is pinned and k=3/4 (I/L) Figure 4.69

    Distribution factor (DF) for DC=

    ?. ?DFs= 1.0

    Distribution factor (DF) for DF= ?

    Thestructureandthedistributionfactorscanberepresentedintabularform,asshowninFigure

    4.91.

    Figure4.91

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    Thedistributionfactorforfixedsupportsisequaltozerosinceanymomentisresistedbyanequal

    andoppositemomentwithinthesupportandnobalancingisrequired.Inthecaseofpinned

    supportsthedistributionfactorisequalto1.0since100%ofanyappliedmoment,e.g.bya

    cantileveroverhang,mustbebalancedandacarryoverof1/2xthebalancingmomenttransferred

    totheremoteendattheinternalsupport.

    Step3

    Thefixedendmomentsarenowenteredintothetableattheappropriatelocations,takingcareto

    ensurethatthesignsarecorrect.

    Step4

    Whenthestructureisrestrainedagainstrotationthereisnormallyaresultantmomentatatypical

    internalsupport.Forexample,considerthemomentsC:

    Theoutofbalancemomentisequaltothealgebraicdifferencebetweenthetwo:

    Iftheimposedfixityatonesupport(allothersremainingfixed),e.g.supportC,isreleased,thebeam

    willrotatesufficientlytoinduceabalancingmomentsuchthatequilibriumisachievedandthe

    momentsMCAandMCDareequalandopposite.TheapplicationofthebalancingmomentisdistributedbetweenCAandCDinproportiontothedistributionfactorscalculatedpreviously.

    MomentappliedtoCA=+(48.89x0.4)=+19.56kNm

    MomentappliedtoCD=+(48.89x0.6)=+29.33kNm

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    AsindicatedinSection4.7.2,whenamomentisappliedtooneendofabeamwhilsttheremoteend

    isfixed,acarryovermomentequalto(1/2xappliedmoment)andofthesamesignisinducedatthe

    remoteend.Thisisenteredintothetableasshown.

    Step5

    Theprocedureoutlineaboveisthencarriedoutforeachrestrainedsupportinturn.Thereader

    shouldconfirmthevaluesgiveninthetableforsupportD.

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    Ifthetotalmomentsateachinternalsupportarenowcalculatedtheyare:

    MCA=(+4.44+19.56)=+24.0kNm

    Thedifference=?kN.m

    MCD=( 53.33+29.33+0.62)=?kNm i.e.thevalueofthecarryovermoment

    MDC=(+53.33+14.67+1.24)=?kNm

    Thedifference=?

    MCD=( 70.34+1.10)= 69.24kNm

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    Itisevidentthatafteroneiterationofeachsupportmomentthetruevaluesarenearerto23.8kNm

    and69.0kNmforCandDrespectively.Theexistingoutofbalancemomentswhichstillexist,0.62

    kNm,canbedistributedinthesamemannerasduringthefirstiteration.Thisprocessiscarriedout

    untilthedesiredlevelofaccuracyhasbeenachieved,normallyafterthreeorfouriterations.

    Aslightmodificationtocarryingoutthedistributionprocesswhichstillresultsinthesameanswersis

    tocarryoutthebalancingoperationforallsupportssimultaneouslyandthecarryoveroperation

    likewise.Thisisquickerandrequireslesswork.Thereadershouldcompleteafurtherthree/four

    iterationstothesolutiongivenaboveandcomparetheresultswiththoseshowninFigure4.92.

    *Thefinalcarryover,tothefixedsupportonly,meansthatthisvalueisoneiterationmoreaccurate

    thantheinternaljoints.

    Figure4.92

    ThecontinuitymomentsareshowninFigure4.93.

    Figure4.93

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    Thesupportreactionsandthebendingmomentdiagramsforeachspancanbecalculatedusing

    superpositionasbeforebyconsideringeachspanseparately.

    i. FixedSupportReactions

    ConsiderspanAC:

    Considertheverticalequilibriumofthebeam:

    ConsiderspanCD:

    Considertheverticalequilibriumofthebeam:

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    ConsiderspanDF

    Considertheverticalequilibriumofthebeam:

    Fixedverticalreactions

    Thetotalverticalreactionateachsupportduetothecontinuitymomentsisequaltothealgebraicsumofthecontributionsfromeachbeamatthesupport.

    ii. Freebendingmoments

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    ConsiderspanAC:

    Considertheverticalequilibriumofthebeam:

    ConsiderspanCD:

    Considertheverticalequilibriumofthebeam:

    Considerspan

    DF

    Considertheverticalequilibriumofthebeam:

    Verticalreactionforfreebendingmomentcondition

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    Thefinalverticalsupportreactionsaregivenby(i)+(ii):

    Checktheverticalequilibrium:Totalverticalforce=+2.58+41.81+109.33+36.28

    =+190kN(=totalappliedload)

    ThefinalbendingmomentdiagramisshowninFigure4.94.

    Figure4.94

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    4.7.11Problems:MomentDistribution ContinuousBeams

    AseriesofcontinuousbeamsareindicatedinProblems4.28to4.32inwhichtherelativeEIvalues

    andtheappliedloadingaregiven.Ineachcase:

    i. determinethesupportreactions,ii. sketchtheshearforcediagram and

    iii. sketchthebendingmomentdiagram

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