Properties of Material Teknik

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    INTRODUCTION

    ENGINEERING MATERIAL(MATERIAL TEKNIK)

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    KLASIFIKASI MATERIALENGINEERING MATERIAL CLASSIFICATION)

    LOGAM

    NON

    LOGAM

    LOGAM

    FERRO

    LOGAM

    NON FERRO

    Besi (Fe)Baja karbonBesi cor

    Baja paduan

    Baja tahan karatBaja perkakasBaja ManganBaja icke!Baja SiBaja "hro#d!!

    A!u#iniu# (A!)Te#baga ("u) icke! ( i)Magnesiu# (Mg)Titaniu# (Ti)"oba!t ("o)Seng ($n)"ad#iu# ("d)Ti#ba! (%b)$irkoniu# ($r)

    d!!%o!i#er & %o!i#er a!a#

    & %o!i#er BuatanKera#ik ( high Te#perature Materia!)

    Ko#posit ' MM" (Meta! Matri "o#posite)' Ad anced Materia!

    ' FR% (Fiber rein*orced %!astic)

    KLASIFIKASI material untuk keperluanteknik

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    Logam (Metal)Sifat logam:Daya hanta li!t i" #an $ana! %ai"Ke"&atan elatif tinggiKe"a"&an (!ti'ne!!) yang tinggiUletMam$& %ent&" yang %ai"

    Tahan te ha#a$ im$a"MENGKILA ILA DI GOSOK

    Metalic bonding

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    olimeSifat $olime :

    Daya hanta li!t i" #an $ana!en#ahKe"&atan elatif en#ahEla!ti!ita! tinggi

    UletMam$& %ent&" yang %ai"

    Covalent bond

    Ionic bond

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    Ke ami" Sifat:

    K&at Ke a! Sangat geta!

    Sifat hanta li!t i" * $ana! en#ah

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    Kom$o!it

    Mate ial yang te #i i #a i #&a ata& le%ihmate ial+ Sifat:

    Ringan K&at Ulet Ke"&atannya le%ih tinggi #a i mate ial mat i"!nya

    Kom$onen:

    Mat i"! : mate ial in#&"Reinfo ,ing agent: mate ial$eng&at

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    -eni! "om$o!it

    Komposit matrik logam (MMC) :#ig&na"an &nt&" "om$onen te tent& yang !ifatme"ani"nya en#ah+

    Komposit matrik polimer (PMC) :"e"e a!an #an "e"&atan en#ah teta$i "e&letannya tingi!ehingga #engan $eng&at logam "e"&atan #an"e"e a!annya mening"at

    Komposit matrik keramik (CMC) :"e"e a!an #an "egeta!annya tinggi !ehingga#engan $eng&at logam ting"at "e&letannyamening"at+

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    Contoh "om$o!it

    &

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    !em on &o

    anya" #ig&na"an #i%i#ang ele"t oni"a Sifat:

    Sangat geta! Daya hanta li!t i"nya #a$at #i "ont ol Meng&%ah !ina li!t i" "e ,ayaha #an !e%ali"nya

    A$li"a!i #alam %i#ang ele"t oni"a Tan!i!to Dio#a Inte g ate# Ci ,&it (IC)

    $ ! !

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    o$e e! o ma e a ! amate ial)

    Sifat Me"ani"

    Sifat .i!i!

    Sifat Kimia

    Sifat Ta"nologi

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    Sifat me"ani"

    Sifat logam yang #i"ait"an #engan"ela"&an logam te !e%&t /i"a #i%e%ani#engan %e%an me"ani"+

    Contoh:

    Ke"&atan ta i" (ten!ile !t ength)+ Ke"e a!an (ha #ne!!) Ke"&atan ge!e (!hea !t ength)

    0a ga yang #i$e oleh me &$a"an ha!il

    $eng&/ian !$e!imen #i la%o ato i&m(#ila"&"an $a#a "on#i!i te tent&)+

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    Mo#e! of loa#ing an# !tate! of !t e!!

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    T !il ! !!3! i & 4 ! f i !2 l! #

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    Ten!ile !t e!!3!t ain ,& 4e! fo ,e ami,!2 metal! an#$olyme !

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    Pure Tension Pure Compression

    Pure Shear

    Pure Torsional Shear

    e =

    F normal

    Ao

    e =

    l lo

    lo

    e =

    F shear

    Ao

    = tan

    stress

    strain

    stress

    strain

    e = G

    e = E Elasticresponse

    Elasticresponse

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    Simple tension: cable

    o =

    .A

    Simple shear: drive shaft

    Ao 5 , o!! !e,tionalA ea (6hen &nloa#e#)

    ..

    o =

    . !

    A

    Note: 5 M7A, R he e+

    S"i lift ($hoto ,o& te!y +M+ An#e !on)

    M

    MAo

    8R

    .!A,

    Common States of Stress

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    ( c ) + , , - B r o o k s .

    " o ! e / a

    d i i s i o n o *

    T h o # s o n

    L e a r n i n g / I

    n c 0

    T h o # s o n

    L e a r n i n g 1

    i s a

    t r a d e # a r k u s e d

    h e r e

    i n u n

    d e r !

    i c e n s e 0

    Figure. A unidirectional force is applied to a specimen in the tensiletest by means of the moveable crosshead. The cross-head movementcan be performed using screws or a hydraulic mechanism

    gaugelength

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    Test Specimen Standard

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    Properties Obtained from the TensileTest

    Elastic limit

    Tensile strength, Necking

    Hookes lawPoissons ratio

    Modulus of resilience ( E r

    Tensile toughness

    !uctilit"

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    (c)+,,- Brooks."o!e/ a di ision o* Tho#son Learning/ Inc0Tho#son Learning 1 is a trade#ark used herein under !icense0

    Figure. The stress-strain curve for analuminum alloy

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    (c)+,,- Brook s."o!e/ a di ision o* Tho#son Learning/ Inc0 Tho#son Learning 1 is a trade#ark used herein under !icense0

    Figure. (a) etermining the !."# offset yield strength in gray cast ion$and (b) upper and lower yield point behavior in a low-carbon steel

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    ( c ) + , , - B r o o k s .

    " o ! e / a

    d i i s i o n o *

    T h o # s o n

    L e a r n i n g / I

    n c 0

    T h o # s o n

    L e a r n i n g

    1 i s

    a t r a d e # a r

    k u s e

    d h e r e

    i n u n

    d e r !

    i c e n s e 0

    Figure. %omparison of theelastic behavior of steel andaluminum. For a given stress$aluminum deforms elasticallythree times as much as doessteel

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    cup-and-cone fracture in Al

    brittle fracture

    Figure. Localized deformation of a ductile material duringa tensile test produces a necked region

    (c)+,,- Brook s."o!e/ a di ision o* Tho#son Learning/ Inc0 Tho #son Learning 1 is atrade#ark used herein under !icense0

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    34

    9 Ma im&m $o!!i%le enginee ing !t e!! in ten!ion+

    Metals: occurs hen nec!ing starts" Ceramics: occurs hen crac! propagation starts" Pol#mers: occurs hen pol#mer bac!bones are aligned and about to brea!"

    $%ltimate& Tensile Strength'( TS

    y

    strain

    Ty$i,al e!$on!e of a metal

    F ) fracture orultimatestrength

    *ec! + actsas stressconcentrator

    e n g

    i n e e r

    i n g

    TS

    s t r e

    s s

    engineering strain

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    Deformation Process DuringTest

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    Hardness of Materials

    Hardness test # Measures the resistance of a material topenetration b" a sharp ob$ect%

    Macrohardness # O&erall bulk hardness of materialsmeasured using loads ' N%

    Microhardness Hardness of materials t"picall" measuredusing loads less than N using such test as )noop(H) %

    Nano#hardness # Hardness of materials measured at *+

    * nm length scale using e-tremel" small (.* /Nforces%

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    Kekerasan juga didefinisikan sebagai kemampuan suatu material untukmenahan beban identasi atau penetrasi (penekanan). Didunia teknik,umumnya pengujian kekerasan menggunakan 4 macam metodepengujian kekerasan, yakni !. "rinnel (#" $ "#%)&. 'ock ell (#' $ '#%). *ikers (#* $ *#%)4. +icro #ardness (%amun jarang sekali dipakai red)

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    ,esistance to permanentl# indenting the surface"

    arge hardness means: --resistance to plastic deformation or crac!ing in compression" --better ear properties"

    e+g+2;

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    GAM AR MACAM@MACAM MEDIA ENGU-IAN

    "'-% //'01K2 // *-1K '3

    %ntu! pengu/ian 0ic!ers' belum dila!u!an 1 dipra!ti!um!an"

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    42

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    (c)+,,- Broo ks."o!e/ a di ision o* Tho#son Learning/ Inc0 Tho#so n Learning 1 is a trade#ark used herein under !icense0

    Figure. &ndentors for the 'rinell and oc well hardness tests

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    Pengu/ian !e!erasan 2rinell merupa!an pengu/ian standard secara industri' tetapi !arenapene!ann#a terbuat dari bola ba/a #ang beru!uran besar dan beban besar' ma!a bahan luna!atau !eras se!ali tida! dapat diu!ur !e!erasann#a"

    Rockwell Superficial Hardness Test Block

    Hardness Scale Part No: Penetrator Load Ranges Material

    15N Scale 3! %!5 % Diamond ! Kg 6ll 3teel

    3 N Scale 3 5%!5 % Diamond 5 Kg 6ll 3teel

    !5N Scale 34 %!5 % Diamond 4 Kg 6ll 3teel

    15T Scale 3! 7!5 !$!89 "all ! Kg 6ll "rass

    3 T Scale 3 57!5 !$!89 "all 5 Kg 6ll "rass

    !5T Scale 34 7!5 !$!89 "all 4 Kg 6ll "rass

    15" Scale 3! 2!5 !$:9 "all ! Kg 6ll "rass

    3 " Scale 3 52!5 !$:9 "all 5 Kg 6ll "rass

    !5" Scale 34 2!5 !$:9 "all 4 Kg 6ll "rass15# Scale 3! ;!5 !$49 "all ! Kg 6ll "rass

    3 # Scale 3 5;!5 !$49 "all 5 Kg 6ll "rass

    !5# Scale 34 ;!5 !$49 "all 4 Kg 6ll "rass

    15$ Scale 3!

    3 $ Scale 3 5

    !5$ Scale 34

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    Skala Penekan

    BebanSkala

    Kekerasan Warna AngkaA2a! 3ta#a 4u#!ah

    A

    B"5EF67K LM%R S8

    Kerucut Intan 9+,:

    Bo!a Baja 9/;)Kerucut Intan 9+,:Kerucut Intan 9+,:Bo!a Baja -/9?; ## (9.)Bo!a Baja 9/;)Bo!a Baja 9/;)Bo!a Baja -/9?; ## (9.)Bo!a Baja -/9?; ## (9.)Bo!a Baja =/-; ## (9.@>)Bo!a Baja =/-; ## (9.@>)Bo!a Baja =/-; ## (9.@>)Bo!a Baja 9+/? ## (9.+>)Bo!a Baja 9+/? ## (9.+>)Bo!a Baja 9+/? ## (9.+>)

    9,

    9,9,9,9,9,9,9,9,9,9,9,9,9,9,

    ;,

    ,9@,

    ,,;,

    9@,;,

    9@,;,,

    9@,;,,

    9@,

    =,

    9,,9;,9,,9,,=,

    9;,=,

    9;,=,

    9,,9;,=,

    9,,9;,

    9,,

    9-,9,,9,,9-,9-,9-,9-,9-,9-,9-,9-,9-,9-,9-,

    7ita#Merah7ita#7ita#MerahMerahMerahMerah

    MerahMerah Merah

    MerahMerahMerahMerah

    Sedang!an pengu/ian ,oc! ell coco! untu! semua material #ang !eras dan #ang luna!'penggunaann#a sederhana dan pene!anann#a dapat dila!u!an dengan leluasa" Tabel di

    ba ah menun/u!!an bagaimana memilih s!ala roc! ell"

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    Pada Tabel ditun/u!!an s!ala !e!erasan A' 2 dan C adalah untu! bahan logam' s!ala A dapatdipa!ai untu! bahan sangat !eras seperti 3arbida tungsen" S!ala 4 dan di ba ahn#a dipa!aiuntu! batu gerinda sampai plasti!"

    Pengu/ian ,oc! el superfisial memperguna!an beban #ang ringan untu! memperbai!i !etelitiandari pene!an dengan cara penggunaan #ang sama' /uga dapat mengu!ur !e!erasan permu!aandari bahan #ang di!eras!an !ulitn#a"

    5ambar di ba ah ini menun/u!!an u!uran perbandingan dari pene!anan pada pengu/ian bahan#ang sama dengan berbagai pengu/ian !e!erasan"

    "rinell"ola "aja !5 mm"eban 55 Kg

    'ock ell=enekan 1, ! 5 Kg

    'ock ell=enekan %, 5 Kg

    =ermukaan

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    0ic!ers 3noop

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    Contoh Sifat me"ani": Ke"e a!an

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    0train 1ate Effects and 2mpact3eha&ior

    2mpact test # Measures the abilit" of a material to absorbthe sudden application of a load without breaking%

    2mpact energ" # The energ" re4uired to fracture astandard specimen when the load is applied suddenl"%2mpact toughness # Energ" absorbed b" a material,usuall" notched, during fracture, under the conditions ofimpact test%

    5racture toughness # The resistance of a material tofailure in the presence of a flaw%

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    (c)+,,- Brook s."o!e/ a di ision o* Tho#son Learning/ Inc0 Tho #son Learning 1 is a trade#ark used herein under !icense0

    Figure. The impact test* (a) The %harpy and &+od tests$ and (b)dimensions of typical specimens

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    ( c ) + , , - B r o o k s .

    " o ! e / a

    d i i s i o n o *

    T h o # s o n L e a r n

    i n g /

    I n c 0

    T h o # s o n

    L e a r n i n g

    1 i s

    a t r a d e # a r

    k u s e

    d h e r e

    i n u n

    d e r !

    i c e n s e 0

    Figure. esults from aseries of &+od impacttests for a super-tough nylon

    thermoplasticpolymer,AT &A /AN01%T& A2AT, N3A & ' & TT'& A ' A A 2A AT ,42 AT1N 0AT&F

    Cha $y Te!t S$e,imen!

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    ( c ) + , , - B r o o k s .

    " o ! e / a

    d i i s i o n o *

    T h o # s o n

    L e a r n i n g / I

    n c 0

    T h o # s o n

    L e a r n i n g

    1 i s

    a t r a d e # a r

    k u s e d

    h e r e

    i n u n

    d e r !

    i c e n s e 0

    Figure. The %harpy 5-notch properties for a'%% carbon steel and aF%% stainless steel. TheF%% crystal structuretypically leads tophigher absorbedenergies and notransition temperature

    Figure.The area contained within the

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    ( c ) + , , - B r o o k s .

    " o ! e / a

    d i i s i o n o *

    T h o # s o n

    L e a r n i n g / I

    n c 0

    T h o # s o n

    L e a r n i n g 1 i s

    a t r a d e # a r

    k u s e d

    h e r e

    i n u n

    d e r !

    i c e n s e 0

    true stress-true strain curve is relatedto the tensile toughness. Althoughmaterial B has a lower yield strength$ itabsorbs a greater energy than material A . The energies from these curves maynot be the same as those obtained from

    impact test data

    f

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    Sifat 1!i! Sifat 1!i" !&at& %ahan a#alah

    "emam$&an !&at&%ahan7mate ial #itin/a& #a i!ifat 1!i"nya+

    Contoh: Ke a$atan ma!!a (#en!ity) Titi" leleh (melting $oint) enam$ilan (a$$ea an,e)

    Metal or allo% kg&cu'(

    titanium 4. 55

    cast iron8.:55

    >.:55

    steel stainless >.4:5 :.555

    iron >.: 5

    copper :.? 5

    sil@er !5.4?5

    lead !!. 45

    uranium !:.?55

    gold !?. &5

    tungsten !?.855

    plutonium !?.:55

    platinum &!.455

    Sifat "imia

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    Sifat "imia Ketahanan !&at& mate ial te ha#a$

    ea"!i "imia yang te /a#i #i!e"ita nya

    Contoh : Ketahanan te ha#a$ "a at (,o o!ion

    e!i!tan,e) Ketahanan te ha#a$ $ana!

    .lamma%ility

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    Sifat 1!i!: !t &"t& mi" o

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    SI AT KIMIA: Ko o!i

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    SI.AT KIMIA: Ko o!iKorosi : Peristiwa

    perusakan atau degradasimaterial logam akibatbereaksi secara kimiadengan lingkungan

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    Ma,am@ma,am Ko o!i

    itti !i

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    itting ,o o!ion

    Sifat te"nologi

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    Sifat te nologi Kemam$&an !&at& mate ial &nt&"

    #i$ o!e! le%ih lan/&t+ Contoh:

    Mam$& me!in (ma,hinea%ility)

    Mam$& la! (6el#a%ility) Mam$& %ent&" (fo minga%ility)

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    SCC (!t e!! , a," ,o o!ion)

    Sifat te"nologi: 6el#a%ility

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