fiber and composite notez

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    Questions

    1. What are the two phase types for composite materials?1. What are the two phase types for composite materials?

    2. Which factor may2. Which factor mayNOTNOTinfluence properties of composites?influence properties of composites?A. shape of dispersed phase B. amount of dispersed phase

    C. distribution of dispersed phase D. color of disp. phase

    3. What are the strengthening mechanism for large3. What are the strengthening mechanism for large--particleparticle

    composites and dispersion strengthened composites?composites and dispersion strengthened composites?

    Large-particle composites:

    larger than atomic/molecular level

    Dispersion strengthened composite:

    on atomic/molecular level

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    2

    Continuous & aligned fiber composites

    Stress-strain behavior for longitudinal loading

    Schematic stressstrain curve for

    an aligned fiber

    reinforced composite that is exposed to a uniaxialstress applied in the direction of alignment

    Stage I:

    Both fibers and matrix deformelastically, so the stress-strain

    curve is linear.

    Stage II:The fibers continue to stretch

    elastically, the matrix yields and

    deforms plastically.

    The onset of composite failure

    begins as the fibers start to

    fracture, which corresponds to a

    strain off

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    Continuous & aligned fiber composites

    Elastic behavior for longitudinal loadingc = mVm + fVf and c = m = f

    Volume fraction

    Ecl = EmVm + EfVf Ecl = longitudinal modulus

    c : composite

    f : fiberm : matrix

    mm

    ff

    m

    f

    VE

    VE

    F

    F

    Ratio of the load carried by fibers to that by matrix:

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    In transverse loading the fibers carry less of the load

    c= mVm + fVf and c = m = f =

    f

    f

    m

    m

    ct EV

    EV

    E1

    Ect = transverse modulus

    c = composite

    f = fiberm = matrix

    isostress

    Ect

    EmEf

    VmEf VfEm

    Continuous & aligned fiber composites

    Elastic behavior for transverse loading

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    Example Problem 1

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    Example Problem 2

    Compute the elastic modulus of the composite material

    described in Example Problem 1, but assume that the stress is

    applied perpendicular to the direction of fiber alignment.

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    Continuous & aligned fiber composites

    Longitudinal Tensile Strength

    fffmcl VV*'* )1(

    Longitudinal strength of the

    composite

    : stress in the matrix at fiber

    failure;

    : fiber tensile strength

    '

    m

    *

    f

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    Continuous & aligned fiber composites

    Transverse Tensile StrengthThe strengths of continuous and aligned fibrous

    composites are highly anisotropic.

    Along the longitudinal direction, have high TS.

    Along the transverse direction, have low TS.

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    Discontinuous & aligned fiber composites

    Even though reinforcement efficiency is

    lower for discontinuous fibers, discontinuous

    and aligned fiber composites are becoming

    increasingly more important in the

    commercial market.

    Chopped glass fibers are used most

    extensively; however, carbon and aramid

    discontinuous fibers are also employed.

    These short fiber composites can be

    produced hav ing modul i o f e last ic ity

    and tensile strengths that approach 90% and

    50%, respectively, of their continuous

    fiber counterparts.

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    Discontinuous & Random fiber composites

    efficiency factor:

    -- aligned: K = 1 (aligned parallel)

    -- aligned: K = 0 (aligned perpendicular)

    -- random 2D: K = 3/8 (2D isotropy)

    -- random 3D: K = 1/5 (3D isotropy)

    Ecd = EmVm + KEfVf

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    16.13 Assume that the composite described in Problem 16.8

    has a cross-sectional area of 480 mm2 (0.75 in.2) and is

    subjected to a longitudinal load of 53,400 N (12,000 lbf).

    (a) Calculate the fibermatrix load ratio.

    (b) Calculate the actual loads carried by both fiber and matrix

    phases.

    (c) Compute the magnitude of the stress on each of the fiberand matrix phases.

    (d) What strain is experienced by the composite?

    Example Problem 3

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    Fiber Types (diameter, character)

    Whiskers - thin single crystals - large length to diameter

    ratios graphite, silicon nitride, silicon carbide

    high crystal perfection extremely strong, strongestknown

    very expensive and difficult to disperse

    Fibers (small diam.)

    polycrystalline or amorphous

    generally polymers or ceramics Ex: alumina, aramid(), glass, carbon

    Wires (large diam.)

    metals steel, molybdenum, tungsten

    The fiber phase

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    The matrix phase

    Matrix phase:

    The matrix phase of fibrous composites may be a metal,

    polymer, or ceramic. In general, metals and polymers are

    used as matrix materials because some ductility is desirable;for ceramic-matrix composites, the reinforcing component is

    added to improve fracture toughness.

    -- Functions are to:- transfer stress to dispersed phase

    - protect dispersed phase from environment

    - separate fibers and prevent crack propagation

    -- Types:

    Metal-matrix

    Ceramic-matrix

    Polymer-matrix

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    Bonding strengthBonding strength between fiber and matrix is an

    important consideration in the choice of the matrix

    fiber combination.

    The ultimate strength of the composite depends to a large

    degree on the magnitude of this bond; adequate bonding isessential to maximize the stress transmittance from the weak

    matrix to the strong fibers.

    The matrix phase

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    Polymer-matrix composites

    Polymer matrix + fiber reinforcement phase

    used most widely in largest quantities

    Polymer-matrix compositesPolymer-matrix compositesPolymer-matrix compositesPolymer-matrix compositesPolymer-matrix compositesPolymer-matrix composites

    aramid fiber

    carbon fiber

    Polymer-matrix composites

    glass fiber

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    -Glass fiber reinforced polymer composites

    Merits of glass fibers

    1. easily drawn into high-strength fibers

    2. composites be fabricated economically3. relatively strong fiber

    4. used in various corrosive environments

    Limitations

    1. poor stiffness

    2. service temp: < 200 C

    Applications

    automotive and marine bodies,

    industrial floorings

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    Most commonly used in advanced polymer-matrix

    composites.

    Merits of carbon fibers1. highest specific modulus and specific strength

    2. retain high tensile modulus at high temp.

    3. good chemical stability4. a variety of physical and mechanical properties

    5. relatively inexpensive and cost effective

    Applicationssports & recreational equipment,

    aircraft structural components

    -Carbon fiber reinforced polymer composites

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    Typical applications:

    sporting goods, tires, ropes

    -Aramid fiber reinforced polymer composites

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    Metal-matrix composites

    Advantages

    higher operating temp.

    nonflammability greater resistance to degradation by organic fluids

    more expensive than PMCs

    Applications

    automotive engine component, driveshafts

    aerospace industry

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    The fracture toughness maybe improved significantly

    by introducing particles, fibers and whiskers.

    Ceramic-matrix composites

    Carbon-carbon compositesOne of the most advanced and promising materials.

    Matrix & reinforcement: carbon

    Desirable properties

    high-tensile modulus & strength at high temp.

    high fracture toughness

    high thermal conductivity, low thermal expansion

    expensive

    limited: rocket motor, friction materials in aircraft and high-

    performance automobiles

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    Core Problems:

    Self-help Problems:

    Hybrid composites

    Reading: