243-Wikarta-KULIAH v & VII BEAM Gaya Internal, Diagram Gaya Geser Dan Momen

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    KULIAH V & VII

    MEKANIKA TEKNIK TI

    BEAMGAYA INTERNAL, DIAGRAM

    GAYA GESER DAN MOMEN

    OLEH:

    ALIEF WIKARTA, ST

    JURUSAN TEKNIK MESIN

    FTI ITS SURABAYA, 2007

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    Defii!i Be"#

    Beam- structural member designed to support

    loads applied at various points along its length.

    Beam designis two-step process:

    1) determine shearing forces and bending

    moments produced by applied loads2) select cross-section best suited to resist

    shearing forces and bending moments

    Beam can be subjected to concentratedloads or

    distributedloads or combination of both.

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    A$" i% '"(" I%e)"* +

    traight two-force memberABis in

    e!uilibrium under application of Fand

    -F. Internal forcese!uivalent toFand -Fare

    re!uired for e!uilibrium of free-bodies

    ACand CB.

    '"(" I%e)"* : "(" (" #ei-"% .e)!"#" .e).""i."i" !%)-%) !e/i" !%)-%) %e)!e.% #e"1i --/

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    Re"-!i $"1" Be"#

    Beams are classified according to way in which theyare supported.

    "eactions at beam supports are determinate if they

    involve only three un#nowns. $therwise% they are

    statically indeterminate.

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    '"(" 'e!e) 1" M#e $"1" Be"#

    &ish to determine bending moment

    and shearing force at any point in a

    beam subjected to concentrated and

    distributed loads.

    'etermine reactions at supports by

    treating whole beam as free-body.

    (ut beam at Cand draw free-body

    diagrams forACand CB. By

    definition% positive sense for internal

    force-couple systems are as shown.

    rom e!uilibrium considerations%

    determineM and VorMand V.

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    Di")"# '"(" 'e!e) 1" M#e $"1" Be"#

    *ariation of shear and bending

    moment along beam may beplotted.

    'etermine reactions at

    supports.

    (ut beam at Cand consider

    memberAC%22 PxMPV +=+=

    (ut beam atEand consider

    memberEB%

    ( ) 22 xLPMPV +== or a beam subjected to

    concentrated loads% shear is

    constant between loading points

    and moment varies linearly.

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    3%/ S"* 4

    'raw the shear and bending moment

    diagrams for the beam and loading

    shown.

    $+,$/:

    a#ing entire beam as a free-body%

    calculate reactions atBandD.

    ind e!uivalent internal force-couplesystems for free-bodies formed by

    cutting beam on either side of load

    application points.

    0lot results.

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    3%/ S"* 4 5"6"."

    0lot results.

    /ote that shear is of constant value

    between concentrated loads and

    bending moment varies linearly.

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    3%/ S"* 2

    Given: beam is supported

    by a hinge at % a roller at B.

    orce applied at (. oment

    applied at '.

    Find: 'raw the shear and

    bending moment diagrams

    Plan:

    a) 'raw a B' of the beam.

    b)(alculate support reactions.

    c) ind e!uivalent internal force-couple systems for free-bodies formed

    by cutting beam on either side of load application points.

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    3%/ S"* 2 5"6"."

    3y4 5

    y6 By7 855 4 5

    5.1 6 By7 5.8 4 5

    By4 5.9 #ip

    3B4 5

    - y25) 6 5.815) 7 ; 4 5

    25y4 8 - ;

    y4 5.1 #ip

    y By

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    3%/ S"* 2 5"6"."

    0otongan 1-1

    31-14 5

    5.1 7 * 4 5

    * 4 5.1 #ip

    < 4 5 ft *4 5.1 #ip

    < 4 15 ft *(4 5.1 #ip

    31-14 5

    7 5.1

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    3%/ S"* 2 5"6"."

    0otongan 2-2

    32-24 5

    5.1 7 5.8 7 * 4 5

    * 4 5.1 7 5.8 #ip

    * 4 - 5.9 #ip

    < 4 15 ft *(4 - 5.9 #ip

    < 4 19 ft *'

    4 - 5.9 #ip

    32-24 5

    7 5.1

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    3%/ S"* 2 5"6"."

    0otongan =-=

    5.1 #ip 5.9 #ip 0.1 kip15 x < 20 ft

    V

    M

    x

    3=-=4 5

    5.1 7 5.8 7 * 4 5

    * 4 5.1 7 5.8 #ip

    * 4 - 5.9 #ip

    < 4 19 ft *'4 - 5.9 #ip

    < 4 25 ft *'

    4 - 5.9 #ip

    3=-=4 5

    7 5.1

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    3%/ S"* 2 5"6"."

    'iagram >eser dan omen

    31-14 5 4 5.1

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    3%/ S"* 8

    'raw the shear and bending moment

    diagrams for the beamAB. he

    distributed load of ?255 /@m. e

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    3%/ S"* 8 5"6"."

    $+,$/:

    a#ing entire beam as a free-body% calculatereactions atAandB.

    :5= AM

    ( ) ( ) ( ) ( ) ( ) 5m99.5/1A55m19.5/2185mA.5 =B

    /18;2=B

    :5= BM

    ( ) ( ) ( ) ( ) ( ) 5mA.5m29.5/1A55m89.5/2185 =+ A

    /2=1A=

    A

    :5= xF 5=xB

    /ote: he 1A55 / load atEmay be replaced by

    a 1A55 / force and 1A5 /m. couple atD.

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    3%/ S"* 8 5"6"."

    :51 =M ( ) 5?2552=1A 21

    =++ Mxxx

    2=8552=1A xxM =

    :52 =M ( ) 519.521852=1A =++ Mxx

    ( )m/19A=2;

    +=xM

    rom CtoD:

    = :5F 521852=1A = V

    /19A=V

    valuate e!uivalent internal force-couple systems

    at sections cut within segmentsAC% CD% andDB.

    rom to C:

    = :5F 5?2552=1A = Vx

    xV ?2552=1A=

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    3%/ S"* 8 5"6"."

    :52 =M

    ( ) ( ) 5;9.51A551A519.521852=1A =+++ Mxxx

    ( ) m/18;21=1; = xM

    valuate e!uivalent internal force-couple

    systems at sections cut within segmentsAC%

    CD% andDB.

    romDtoB:

    = :5F 51A5521852=1A = V

    /18;2=V

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    3%/ S"* 8 5"6"."

    0lot results.rom to C:

    xV ?255=21A=

    225=21A xxM =

    rom CtoD:

    /19A=V

    ( ) m/19A=2; += xM

    romDtoB:/18;2=V

    ( ) m/18;21=1; = xM

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    3%/ S"* 9

    'raw the shear and bending-moment diagrams

    for the beam and loading shown.

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    3%/ S"* 9 5"6"."

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