ch02- Strain Mekanik Bahan

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    2005 Pearson Education South Asia Pte Ltd

    2. Strain

    1

    CHAPTER OBJECTIVES

    Define concept of

    normal strain

    Define concept of

    shear strain

    Determine normaland shear strain in

    engineering

    applications

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    CHAPTER OUTLINE

    1. Deformation2. Strain

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    Deformation

    Occurs when a force is applied to a body

    Can be highly visible or practically unnoticeable

    Can also occur when temperature of a body is

    changed

    Is not uniform throughout a bodys volume, thus

    change in geometry of any line segment within

    body may vary along its length

    2.1 DEFORMATION

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    To simplify study of deformation

    Assume lines to be very short and located in

    neighborhood of a point, and

    Take into account the orientation of the line

    segment at the point

    2.1 DEFORMATION

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    Normal strain

    Defined as the elongation or contraction of a linesegment per unit of length

    Consider lineABin figure below

    After deformation, schanges to s

    2.2 STRAIN

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    Normal strain

    Defining average normal strainusing avg(epsilon)

    As s 0, s 0

    2.2 STRAIN

    avg=s s

    s

    =

    s s

    s

    lim

    BA along n

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    Normal strain

    If normal strain is known, use the equation to

    obtain approx. final length of a shortline segment

    in direction of nafter deformation.

    Hence, when is positive, initial line will elongate,if is negative, the line contracts

    2.2 STRAIN

    s (1 + )s

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    2.2 STRAIN

    Units

    Normal strain is a dimensionless quantity, asits a ratio of two lengths

    But common practice to state it in terms ofmeters/meter (m/m)

    is small for most engineering applications, sois normally expressed as micrometers permeter (m/m)where1m = 106

    Also expressed as a percentage,e.g.,0.001 m/m = 0.1 %

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    2.2 STRAIN

    Shear strain

    Defined as the change in anglethat occurs

    between two line segments that were originally

    perpendicularto one another

    This angle is denoted by (gamma) andmeasured in radians (rad).

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    2.2 STRAIN

    Shear strain

    Consider line segmentsABandACoriginating

    from same pointAin a body, and directed along

    the perpendicular nand taxes

    After deformation, lines become curves, such thatangle between them atAis

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    2.2 STRAIN

    Shear strain

    Hence, shear strain at pointAassociated with n

    and taxes is

    If is smaller than /2, shear strain is positive,otherwise, shear strain is negative

    nt=

    2

    lim

    BA along n

    C A along t

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    Cartesian strain components

    Using above definitions of normal and shear strain,

    we show how they describe the deformation of the

    body

    2.2 STRAIN

    Divide body into smallelements with

    undeformed dimensions

    ofx,yandz

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    Cartesian strain components

    Since element is very small, deformed shape of

    element is a parallelepiped

    Approx. lengths of sides of parallelepiped are

    (1 + x) x (1 + y)y (1 + z)z

    2.2 STRAIN

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    Cartesian strain components

    Approx. angles between the sides are

    2.2 STRAIN

    2 xy

    2 yz

    2 xz

    Normal strains cause a change in its volume

    Shear strains cause a change in its shape

    To summarize, state of strain at a point requires

    specifying 3 normal strains; x, y, zand 3 shear

    strains of xy,yz,xz

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    Small strain analysis

    Most engineering design involves applications

    for which only small deformationsare allowed

    Well assume that deformations that take place

    within a body are almost infinitesimal, so normalstrainsoccurring within material are very small

    compared to 1, i.e.,

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    Small strain analysis

    This assumption is widely applied in practical

    engineering problems, and is referred to as

    small strain analysis

    E.g., it can be used to approximate sin = , cos= and tan = , provided is small

    2.2 STRAIN

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    2 St i

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    EXAMPLE 2.1 (SOLN)

    (a) Since normal strain reported at each point along

    the rod, a differential segment dz, located at

    positionzhas a deformed length:

    dz = [1 + 40(103)z1/2] dz

    2 St i

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    EXAMPLE 2.1 (SOLN)

    (a) Sum total of these segments along axis yields

    deformed length of the rod, i.e.,z = 0 [1 + 40(103)z1/2] dz

    = z+ 40(103)(z3/2)|0= 0.20239 m

    0.2 m

    0.2 m

    Displacement of end of rod is

    B= 0.20239 m 0.2 m = 2.39 mm

    2 St i

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    EXAMPLE 2.1 (SOLN)

    (b) Assume rod or line segment has originallength of 200 mm and a change in length of

    2.39 mm. Hence,

    avg=s s

    s =2.39 mm

    200 mm = 0.0119 mm/mm

    2 St i

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    EXAMPLE 2.3

    Plate is deformed as shown in figure. In this

    deformed shape, horizontal lines on the on plate

    remain horizontal and do not change their length.

    Determine

    (a) average normal strainalong sideAB,

    (b) average shear strain

    in the plate relative toxandyaxes

    2 St i

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    EXAMPLE 2.3 (SOLN)

    (a) LineAB, coincident withyaxis, becomes line

    AB after deformation. Length of lineAB is

    AB = (250 2)2+ (3)2 = 248.018 mm

    2 St i

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    EXAMPLE 2.3 (SOLN)

    (a) Therefore, average normal strain forABis,

    = 7.93(103) mm/mm

    (AB)avg= AB

    AB AB 248.018 mm 250 mm250 mm

    =

    Negative sign means

    strain causes a

    contraction of AB.

    2 Strain

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    EXAMPLE 2.3 (SOLN)

    (b) Due to displacement ofBtoB, angle BACreferenced fromx,yaxes changes to .

    Since xy= /2 , thus

    xy= tan13 mm

    250 mm 2 mm = 0.0121 rad( )

    2 Strain

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    CHAPTER REVIEW

    Loads cause bodies to deform, thus points inthe body will undergo displacements or

    changes in position

    Normal strainis a measure of elongation orcontraction of small line segment in the body

    Shear strainis a measure of the change inangle that occurs between two small line

    segments that are originally perpendicular to

    each other

    2 Strain

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    CHAPTER REVIEW

    State of strain at a point is described by sixstrain components:

    a) Three normal strains: x, y, z

    b) Three shear strains: xy, xz, yz

    c) These components depend upon the orientation ofthe line segments and their location in the body

    Strain is a geometrical quantity measuredby experimental techniques. Stress in body

    is then determined from material property

    relations

    2 Strain

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    CHAPTER REVIEW

    Most engineering materials undergo smalldeformations, so normal strain