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      Static load design  1 

    Fx

    FY

    FZ

    Design for Static Load

    ObjectiveStrengthen the knowledge: static and strength of material.Know how to do analysis on component under static loadFind the relationship between these topicsKnow how to use Table in appendix A

    Notation

     Axis: Right Hand Rule  To maintain the position of X, Y and Z axis

      To show the rotation direction of Moment and Torsion

    Force: arrow with single headEg: Fx = 10 kN, Fy = 20 kN and Fz = 30 kN

    F = (10i + 20j + 30k) kN

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    Moment and torsion: arrow with two head on direction of rotation.Eg: Mx = 10 Nm, My = 20 Nm and Mz = 30 Nm

    M = (10i + 20j + 30k) Nm

     Are torsion and moment same and why they are named differently?

    `

    Mx

    My

    Mz

     

    Mx 

    My 

    Mz 

    Mx 

    My 

    Mz 

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      Static load design  3 

    Static:

        000  z  y x   F  F  F   

        000  z  y x   M  M  M   

    Discuss the following problem

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      Static load design  4 

    Based on T, which one has higher force value (F1 or F2). If pulleydiameter is D, find F1 in function of D and T.

    Find F1 in function of D (sprocket diameter) and d (pulley diameter)

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    Pulley

    Chain

    Sprocket

    Ball Bearing

    V-Belt

    F=600 N

    F1=1.75F2

    F2Shaft rotated at

    350 rpm (ccw)

    F=600 N

    Isometric View 

    1.  3-80 pp 140

    2.  3-84 pp 140

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    3.  3-68 pp 137

    FBD Figure 3-72, 3-73

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    INDETERMINATE PROBLEM

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    STRESS ANALYSIS

     Axial Load (P)

     Axial Stress A

     P   

     

     A: cross sectional area

    Stresses on element

    Shear load (V) : can be neglected when the part is subjected tobending or torsion

    Transverse shear stress A

    V   

     

     A: cross sectional area

    P

     V

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    Moment

    Bending stress

     Z 

     M 

     I 

     Mc  

     

    c: distance from the center axisI: second moment of area (last page, Table

     A-6 to A-8 pp1008 - 1012)Z: section modulus (Table A-6 to A-8)

    Stresses on element

    M

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    Torsion

    Note:In design we are responsible our design is safe against failure.Therefore, parameters such A, I, Z and J play important role as wellas the loads themselves.

    NoteWe should identify the most critical element in order to proceed withour analysis.

    We should calculate the maximum stresses resulted from stress onthe element of the most the critical position. How?

    Shear Stress J Tr     

    R: distance from center axisJ: second polar of momentinertia

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    Compounded Load

    P M Compounded

    Which element is most critical and why?

     A

    B, D

    C

     A

    B, D

    C

     A

    B, D

    C

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    T M Compounded

    Which element is most critical and why?

    M T 

     A

    B, D

    C

     A

    B, D

    C

     A

    B, D

    C

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    M1 M2 Compounded

    Which element is most critical and why?

    M1 

    M1 

    M2 

    M2 

     A

    B, D

    C

     A

    B, D

    C

     A

    B, D

    C

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    Mohr CircleMohr Circle is used to represent graphically the state of stress on theentire structure.

    Element

    Refer to Eq 3-13, 3-14 pp 77, 78 to calculate the principal stressRead Mohr Circle background theory: Section 3-6 (pp 70 – 84)

    τxy

    sxy

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    STATIC FAILURE THEORIES (Chap 5) 

    Ductile materials (yield criteria) Maximum shear stress (MSS): Sec 5-4 pp 211 Distortion energy (DE): Sec 5-5 pp 213 Ductile Coulomb-Mohr (DCM): Sec 5-6 pp 219

    Brittle materials Maximum normal stress (MNS) Sec 5-8 Brittle Coulomb-Mohr (BCM) Sec 5-9

     Modified Mohr (MM) Sec 5-9

    Maximum shear stress Theory (MSS)

     Yielding begins whenever the maximum shear stress in any elementequals or exceeds the maximum shear stress in a tension test

    specimen of the same material when that specimen begins to yield.

    LIMIT DUE YIELDING

    LIMIT

    DUET

    O

    SHEAR

    SytSyc

     

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    Therefore, any Mohrcircle generated fromthe most critical element

    must lie inside this limit

    Failure occurs when the Mohr

    circle lies outside the limits

    When the limits are plotagainst sa and sb.

    Case1: when sa and sb are +ve

    Case2: when sa is +ve and sb is –ve

    Case3: when sa and sb are -ve

    Syt Syc 

    SytSyc

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    Case 1 

    Case 2 

    Case 3 

    QA 

    QB 

    Sy 

    Sy 

    Syc 

    Syc 

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    Distortion Energy Theory (DE)

    The effective stress is called Von Misses

    222

    22

    3'

    '

     xy y y x x

     B B A A

                

              

     

    If sy = 0

    223'  xy x             

    Therefore failure happens when s’ > Sy. To plot the graph sa against sb for DE Theory, s’ = Sy.

    QA 

    QB

    Sy

    Sy

    Syc

    Syc

     

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    Load line and its meaning on MSS and DE.Line when it is drawn from (0, 0) to another point and this line acrossthe (sa, sb) of the Mohr Circle of the element.Intersection between load line and the MSS and DE Curve: point of

    yielding according the theories defn. Any stresses exceed theseintersecting point is considered fail due to yielding ( FS < 1 ).Before the intersection point ( FS > 1)

     At the intersection point (FS = 1)Beyond the intersection point ( FS < 1 )  NO GO

    Pure Shear LineWhen the element is subject to shear only. The intersection of this

    line with MSS and DE curve will remark the relationship between yieldstress and shear yield stress. ThereMSS : Ssy = 0.5 SyDE: Ssy = 0.577 Sy

    s A 

    sB 

    Sy 

    Syc 

    Syc 

    Pure Shear Ln 

    Load Line 

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    Static failure using mathematical approach

    Three-dimensional Stresses (Section 3-7 pp 82)

    Principal Stresses s3 < s2 < s1Maximum Shear Stress

    When there is no pressure, sz is equal to zero, therefore one of

    principal stress must equal to zero.

    τ xy

    s xy

    s1s2s3

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    What is the value of s3, s2, s1 and τmax for a, b and c?

    MSST theory

    Maximum shear 2

    31

    max

        

      

     

     Allowable shear stress n

    S S 

      y

     sy2

     

    Safety factor31       

     

      yS n

     

    DET

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    Total stress22

    3'  xy x             

    22'  B B A A                 

    Safety factor '  

     yS n 

     

    *NOTEPlease differentiate between

      stresses on element  xy x        ,

     

      2D Principal stresses  B A         ,  

      3D Principal stresses 321   ,,           

    Brittle Material

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    Note:Please take note of the following appendix(All the tables on the appendices should be at your finger tips)

    Table A-6 to A-8

    Table A-9

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    Table A-18

    Table A-20 to A-22