Anbu Mechanical Properties of Dental Materials

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    MECHANICALPROPERTIES

    OF

    DENTAL MATERIALS

    Presented byANBU .ILAI yr P.G student

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    CONTENTS:

    IntroductionForces

    Forces in oral cavity

    Variants of forces

    Stress and Strain

    Types of stress

    Based on Elastic deformation

    Elastic modulus

    Shear modulus

    Flexibility

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    CONTENTS

    Strength properties:

    STRESS-STRAIN CURVE

    Proportional limitElastic limit

    Yield strength

    Ultimate strengthFracture strength

    Flexural strength

    Fatigue strength

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    CONTENTS

    Masticatory forces

    Toughness

    Fracture toughness

    Brittleness

    Ductility and Malleability

    Surface properties:

    Hardness and the tests

    BRINELLROCKWELL

    KNOOP

    VICKERSBARCOL & SHORE

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    INTRODUCTION

    Laws ofMECHANICS

    Based on energy and forces

    Static and dynamic

    mechanical properties:

    Success or failure potentialof any

    prostheses is dependent upon theirmechanical

    properties.

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    deformation:

    Reversible : proportional limit, resilience,

    elastic modulus

    Plastic: hardness, percent elongation

    Combination: yield strength, toughness

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    FORCE Generated by one body interacting with the

    other.

    Results in transformation or deforming.

    Defined by

    1.point of application

    2.magnitude

    3.direction

    Unit Newton (N)

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    Forces in oral cavity Occlusal / masticatory

    Forces on restorations

    Occlusal :

    a) Maximum range 200 -3500 N

    b) Highest biting force 4337 N - 2secs

    c) The average biting forces on permanent teeth

    were 665,450, and 220 N on molars, bicuspids,and incisors respectively

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    FORCES

    On/by the Restoration :

    Removable partial denture 65 235 N.(rpd)

    FIXED 40% of the natural dentition.

    REMOVABLE OR COMPLETE denture only 15%

    Of the natural.

    Women 90N less than men.

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    FORCES - VARIANTS

    1. Axial (tensile or compressive)

    1. Shear (sliding, rubbing)

    1. Bending (bending movement)

    1. Tortional (twisting movement)

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    FORCES & THEIR DEFORMATION

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    TYPES OFFORCES:

    compressive,

    tensile,

    shear

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    RESULT OF THE APPLIED FORCE

    Compression- two sets of forces directedtowards each other

    Tension - two sets of forces directed away

    from each other in a straight line

    Shear - two sets of forces directed parallel to eachother , but not along the same straight line

    Torsion results from the twisting of the body.

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    STRESS:

    Internal reaction equal in intensity andopposite to the direction of the applied externalload/force

    force/area = F/A

    within a structure

    Dependent on

    a. Strain rate

    b. Shape

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    STRESS:

    Denoted by S or

    Designated as force per unit area ( =N/m )

    Pascal = 1 N / m.

    Commonly stress is reported in terms of

    mega Pascals(MPa)

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    Types of stress

    SIMPLE

    1.tensile

    2.compressive

    3.shear

    COMPLEX

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    Types of stress

    TENSILE STRESS :

    stretch / elongate

    perpendicular to thedirection

    Eg: A sticky candy can be used to removecrowns by means of tensile force

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    Types of stressSHEAR STRESS: force/cross sectional area

    parallel to the direction of theforce

    Application of shear force may produceelastic shear strain or plastic shear strain.

    FLEXURAL STRESS:

    Also called as bending stress.

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    FLEXURAL STRESS

    THREE UNIT BRIDGE & CANTILEVERBRIDGE

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    STRAIN:

    change in length/ unit initial length.

    Relative deformation of an object that issubjected to stress

    It is denoted by

    Designated as L / L.

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    YOUNGs MODULUS:

    relative stiffness (or) rigidity

    elastic stress

    elastic strain

    unit GPa its a constant

    unaffected by the elastic (or)plastic stress

    Independent of the ductility, heat or

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    Enamel - stiffer but

    brittle

    Dentin - flexible

    alsotougher

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    DYNAMIC YOUNGs MODULUS

    in dynamic state of motion

    Velocity of the sound waves

    Ultrasonic transducers and receivers

    Often higher than values by static measurements

    SHEAR modulus: shear stress is induced

    38 % of elastic modulus

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    POISSONs RATIO:

    WITHIN ELASTIC RANGE,

    LATERAL STRAIN

    AXIAL STRAIN

    MORE DUCTILE SOFT GOLD ALLOYS - HIGH

    REDUCTION IN CROSS SECTIONAL AREA ANDHIGHER POISSONS RATIO.

    UNITLESS.

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    STRESS - STRAIN CURVE

    THE MECHANICAL PROPERTIES OF THE

    MATERIAL.

    STRAIN IS PLOTTED OVER X AXIS (horizontal

    axis ) IS AN INDEPENDENT VARIABLE.

    STRESS PLOTTED OVER Y AXIS(vertical axis).

    AS THE STRESS INCREASES STRAIN ALSOINCREASES.

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    STRESS STRAIN CURVE

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    STRESS -STRAIN CURVE

    A. PROPORTIONAL LIMIT & ELASTIC LIMIT

    A. YIELD STRENGTH

    A. ULTIMATE STRENGTH

    A. FRACTURE STRENGTH

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    PROPORTIONAL LIMIT (A) :

    DEFINED AS THE GREATEST STRESS THAT AMATERIAL WILL SUSTAIN WITHOUT DEVIATIONFROM LINEAR PROPOTIONALITY OF STRESS TOSTRAIN WITHOUT PERMANENT DEFORMATION.

    ELASTIC LIMIT:

    IS THE GREATEST STRESS TO WHICH A MATERIAL

    CAN BE SUBJECTED SUCH THAT IT RETURNS TO ITSORIGINAL DIMENSIONS WHEN FORCE IS RELEASED.

    WITHOUT PERMANENT DEFORMATION.

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    YIELD STRENGTH/ YIELD POINT /

    PROOF STRESS (B):

    THE STRESS AT WHICH A MATERIAL

    EXHIBITS A SPECIFIED LIMITINGDEVIATION FROM PROPORTIONALITYOF STRESS TO STRAIN.

    AMOUNT OF PERMANENT STRAIN ISREFERRED TO AS PERCENT OFFSET

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    YIELD STRENGTH:

    ELASTIC LIMIT AND YIELD STRENGTH DEFINESTHE TRANSITION FROM ELASTIC TO PLASTICBEHAVIOUR .

    BEGINSTO FUNCTION IN A PLASTIC MANNER.

    E.g Clasp is bent and the function of it is based

    on elastic recovery within the range and provideretention.

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    ULTIMATE STRENGTH(C):

    COMPRESSIVE STRENGTH :

    Compressive stress at the point of fracture

    TENSILE STRENGTH:

    tensile stress at point of fracture

    YIELD STRENGTH IS IMPORTANTTHAN ULTIMATE STRENGTH BECAUSE ITIS AN ESTIMATE OF WHEN A MATERIAL

    WILL START TO DEFORM PERMANENTLY

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    FRACTURE STRENGTH(D):

    THE STRESS AT WHICH A BRITTLE MATERIALFRACTURES

    MATERIAL DOES NOT FRACTURE AT THE POINTAT WHICH MAXIMUM STRESS OCCURS

    AFTER MAXIMUM TENSILE FORCE - MATERIALELONGATES RESULTING IN NECKING REDUCTION IN CROSS SECTIONAL AREA

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    FRACTURE STRENGTH(D):

    MATERIALS EXHIBITING NECKING, THE

    ULTIMATE & FRACTURE STRENGTH ARE

    DIFFERENT.

    IN DENTAL ALLOYS AND CERAMICS

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    FLEXURAL STRENGTH

    MODULUS OF RUPTURE (or) TRANSVERSE. LOADING A SIMPLE BEAM SUPPORTED (NOT

    FIXED) AT EACH END, WITH A LOAD APPLIED INTHE MIDDLE.

    THREE POINT BENDING TEST .

    IN COMPARING DENTURE BASE MATERIALS INWHICH STRESS OF THIS TYPE IS APPLIED WITH

    THE MASTICATORY FORCES.

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    FATIGUE STRENGTH

    A structure subjected to repeated or cyclic stresses

    well below its ultimate tensile strength can produceabrupt failure.this phenomenon is called fatiguefailure.

    Endurance limit: the maximum stress that can bemaintained without failure over an infinite number ofcycles

    brittle with rough surface fail in fewer cycles.

    Ceramic brackets with activated wires - static fatiguefailure.

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    IMPACT STRENGTH

    ENERGY REQUIRED TO FRACTURE A MATERIALUNDER AN IMPACT FORCE

    1. CHARPY-TYPE IMPACT TESTER2. IZOD IMPACT TESTER

    LOW ELASTIC MODULUS &HIGH TENSILE STRENGTH WILL HAVE

    HIGH IMPACT RESISTANCE

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    TEAR STRENGTH

    Resistance of a material to tearing forces.

    Dental polymers in thin sections

    eg : Flexible impression materials in interproximalareas, maxillofacial materials and soft liners fordentures.

    Rapid removal in alginate impression leads tomaximum tear strength .

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    TEAR STRENGTH

    Material Tearstrength(kN/m)

    Agar duplicating material0.22

    Denture liners

    2.6-45

    Impression materials

    Agar

    0.99

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    FLEXIBILITY

    FLEXIBILITY:

    maximumflexibility is defined asflexural strain occuringwhen material is

    stressed to itsproportional limit.

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    ELONGATION:

    DEFORMATION THAT RESULTS BY TENSILE FORCE .

    WORKABILITYOF THE ALLOY.

    %ELONGATION =INCREASE IN LENGTH X 100%

    ORIGINAL LENGTH

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    ELONGATION:

    % ELONGATION INCLUDES BOTH ELASTIC ANDPLASTIC ELONGATION.

    PLASTIC ELONGATION IS GREATER.

    HIGHER YIELD STRENGTH ,LESS ELONGATION

    Alloy % Elongation

    Gold (type 3) 34.0

    40% Au-Ag-CU 2.0

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    COMPRESSION:

    AMOUNT OF DEFORMATION A MATERIAL CAN

    WITHSTAND BEFORE RUPTURE UNDER

    COMPRESSIVE STRESS - % OF COMPRESSION.

    DUCTILITY AND MALLEABILITYARE

    INDICATED BY ELONGATION AND

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    DUCTILITY :

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    DUCTILITY:

    RELATIVE ABILITY OF THE MATERIAL TO DEFORMPLASTICLLY BEFORE IT FRACTURES.

    ABILITY OF A MATERIAL TO DRAWN IN TO WIRES WHENSUBJECTED TO TENSILE FORCES.

    RELATED TO THE WORKABILITY OF A MATERIAL .

    B.I= DUCTILITY

    YIELDSTRENGTH

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    Measurement of ductility:

    1. Percent elongationafter fracture

    1. Reduction in area of the tensile test

    specimens

    1. Maximum number of the bends in cold blendtest

    . More the ductility, higher the metal can beburnished

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    MALLEABILITY :

    ABILITY OF A MATERIALTO BE HAMMERED ORROLLED IN TO THINSHEETS WITHOUTFRACTURING.

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    DUCTILITY AND MALLEABILITY

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    RESILIENCE

    Relative amount ofelastic energyper unitvolume on unloading is defined as resilience

    Area bounded by elastic region

    Unit mMN/cubic m

    Difference in loading and unloading portion iscalled as hysteresis

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    RESILIENCE

    defined as the amount ofenergy absorbed

    by a structure when it is stressed not toexceed its proportional limit.

    Springiness

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    TOUGHNESS

    IS THE AMOUNT OF ELASTIC AND PLASTIC

    DEFORMATION. ENERGY REQUIREDTOFRACTURE A MATERIAL.

    ABILITY OF A MATERIAL TO ABSORB ELASTICENERGY AND TO DEFORM PLASTICALLY BEFOREFRACTURE.

    AREA UNDER THE ELASTIC AND PLASTICPORTION(TOTAL) OF A STRESS STRAIN CURVE.

    GREATER THESTRENGTH

    AND HIGHER THEDUCTILITY- TOUGHNESS INCREASES.

    FRACTURE TOUGHNESS

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    FRACTURE TOUGHNESS

    Ability to be plastically deformed withoutfracture.

    is a material property & is proportional to the

    energy consumed in plastic deformation.

    Gives a relative value of a materials ability to

    resist crack propagation.

    larger the flaw, lower the stress required tocause the fracture.

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    FRACTURE TOUGHNESS

    Brittle - glass - breaks

    Ductile - copper rod - bends

    Fillers in resin increases it.

    Aging &

    storage decreases the fracture toughness

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    HARDNESS

    RESISTANCE OF THE MATERIAL TO DEFORMPLASTICALLY.

    RELATED TO HARDNESS OF MATERIAL

    COMPRESSIVE STRENGTH,

    PROPORTIONAL LIMIT AND

    DUCTILITY.

    INDICATIVE OF EASE OF FINISHING OF ASTRUCTURE AND ITS RESISTANCE TO

    SCRATCHING

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    TYPES OF HARDNESS TESTS

    MACRO TEST :

    BRINELL

    ROCKWELL

    MICRO TEST :

    VICKERsKNOOP

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    SHAPE OF THE INDENTER

    1

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    BRINELL HARDNESS TEST

    OLDEST

    SMALL STEEL OR TUNGSTEN CARBIDE BALL 1.6mm DIAMETER

    LOAD OF 123N30 sec CONTACT WITH SPECIMEN

    DIAMETER OF INDENTATION IS MEASRURED

    BRINELL HARDNESS NUMBER (BHN)=LOAD/SURFACE AREA OF INDENTATION

    FOR METALS AND ALLOYS

    1

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    ROCKWELL HARDNESS TEST

    RAPID -superficialmethod

    29.4N -294N 10 min

    BALL OR METAL CONEINDENTER

    DEPTH OF INDENTATIONMEASURED WITH A

    SENSITIVE DIALMICROMETER

    GOOD FOR TESTINGVISCOELASTIC MATERIALS

    DISADVANTAGES:

    1

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    KNOOP HARDNESS TEST

    MICRO INDENTATION TEST DIAMONDINDENTING TOOL WITH A PYRAMID SHAPE

    LENGTH OF THE DIAGONAL IS MEASURED

    USED FOR THIN PLASTIC OR METAL SHEETS OR

    BRITTLEMATERIALS.

    ENAMEL ,DENTIN ,METALS (VARY IN HARDNESS)

    1

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    VICKERS HARDNESS TEST

    SQUARE BASED DIAMOND INDENTER WITH136o POINT ANGLE

    DIAGONALS OF THE INDENTATIONMEASURED

    VHN= LOAD/AREA OF PYRAMIDAL

    IMPRESSION

    10-1200N

    1

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    BARCOL HARDNESS TEST

    USED FOR DEPTH OF CURE OF RESINCOMPOSITES

    SPRING LOADED NEEDLE INDENTER WITHDIAMETER OF 1mm

    10% DECREASE = 20% DECREASE IN

    FLEXURAL STRENGTH

    1

    SHORE A HARDNESS TEST

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    SHORE A HARDNESS TEST

    SHORE A DURAMETER

    USED FOR ELASTOMERS

    BLUNT POINTED INDENTER 0.8mm DIAMETERTAPERS TO A CYLINDER OF 1.6mm.

    INDENTER ATTACHED BY A LEVER TO A SCALETHAT IS GRADUATED FROM 0 100 UNITS. IFINDENTER COMPLETELYPENETRATES THESPEICMEN, READING OF 0 IS TAKEN.

    1

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    FRICTION

    Friction is the resistance to the motion of onematerial body over the other.

    Depends on function

    composition

    surface finish

    lubrication

    sliding mechanism in ortho when wire is passedthrough bracket designed for translation

    1

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    WEAR

    Wear is loss of material

    By removal and relocation

    Through contact of two or more material

    Types: AdhesiveCorrosive

    Surface fatigue

    Abrasive

    1

    DIAMETRAL COMPRESSION TEST

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    DIAMETRAL COMPRESSION TESTFOR TENSION

    In this method, the compressive load is placed by a flatplate against the side of a short cylindrical specimen.

    The vertical compressive force along the side of the diskproduce as a tensile stress that is perpendicular to the

    vertical plane that passes through the center of thedisk. Fracture occur along the vertical plane. In thissituation the tensile stress is directly proportional to thecompressive load applied.

    1

    DIAMETRAL COMPRESSION TEST

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    DIAMETRAL COMPRESSION TESTFOR TENSION

    BRAZILIAN TEST

    1. Only for the

    materials whichexhibitpredominantlyelastic deformation

    2. in brittle materialstensile loadingcauses fracture

    3. Amalgam,cements,

    ceramics,stone

    TENSILE STRESS =2P/ DT

    D-DIAMETER,T-THICKNESS,

    P-APPLIED LOAD

    1

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    DIAMETRAL TENSILE STRENGTH

    1

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    COMPRESSSIVE PROPERTIES

    Comparison of amalgam, resin ,cements.

    Under compressive force.

    Length twice that of the diameter -satisfactory

    Iftoo short, cone formation in the ends occurs

    Iftoo long, buckling occurs

    1

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    SHEAR STRENGTH

    maximum stress that a material can withstandbefore failure in a shear mode of loading.

    tested using the punch or push out method.

    to study the interface between the two

    materials Eg: Porcelain fused to metal.

    Shear strength = F/dh

    1

    BOND STRENGTH

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    BOND STRENGTH

    TESTS HAVE BEEN DEVELOPED TO MEASURETHE BOND STRENGTH BETWEEN TWO

    MATERIALS

    CERAMIC METAL,CEMENT TO METALRESIN COMPOSITES AND ADHESIVES TO ENAMEL AND DENTIN.

    THESE BOND STRENGTH VALUES MAY NOT SIMULATE

    THE CLINICAL SITUATION BECAUSE OF DIFFERENCES

    BETWEEN THE GEOMETRY OF THE TEST SPECIMENS AND

    CLINICAL APPLICATION

    1

    BOND STRENGTH

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    BOND STRENGTH

    BOND STRENGTH VALUES TYPICALLY

    OVERESTIMATE THE BOND STRENGTH OBTAINEDIN CLINICAL USAGE .

    BOND STRENGTH PERFORMED IN TENSION

    CANNOTBE DIRECTLY COMPARED TO THOSEDONE IN SHEAR

    1

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    STRESS CONCENTRATION FACTORS

    Flaws or defects

    stress intensity increases with the length of the flaw

    Surface flaws are associated with higher stress

    Minimized by : polished surface

    increased size

    design shouldnot vary abruptly

    brittle material with lower E value

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    VISCOELASTICITY

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    VISCOELASTICITY

    VISCOSITY:RESISTANCE OF A FLUID TO FLOW

    Viscosity =shear stress / shear strain rate

    MATERIALS THAT HAVE MECHANICAL

    PROPERTIES DEPENDENT ON LOADING RATEARE TERMED AS VISCOELASTIC.

    WITH THE PROPERTIES OF ELASTIC SOLID ANDVISCOUS FLUID.

    FLUIDS : NEWTONIAN

    11

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    VISCOELASTICITY

    NEWTONIAN: constant viscosity

    independent of shear rate

    e.g., cements

    PSEUDOPLASTIC: viscosity decreases withincreasing shear rate

    e.g., endodontic cements

    DILATANT: viscosity increases with increasing

    shear rate

    11

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    VISCOELASTICITY

    MOST DENTAL MATERIALS BEGIN TO SET AFTERTHE COMPONENTS HAVE BEEN MIXED ANDTHEIR VISCOSITY INCREASES WITH TIME.

    EXCEPTION, ZOE NEEDS MOISTURE TO SET.

    VISCOSITY INCREASES WITH INCREASING

    TEMPERATURE

    11

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    VISCOELASTICITY

    STRESS RELAXATION IS THE REDUCTIONINSTRESS IN A MATERIAL SUBJECT TOCONSTANT STRAIN .

    CREEP IS THE INCREASE IN STRAIN IN AMATERIAL UNDER CONSTANT STRESS.

    CREEP COMPLIANCE (J) IS DEFINED AS STRAINDIVIDED BY STRESS AT THE GIVEN TIME.

    J= STRAIN

    STRESS

    11

    STRESS ANALYSIS AND DESIGN

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    STRESS ANALYSIS AND DESIGN

    DESIGN SHOULD NOT RESULT IN STRESS ANDSTRAIN THAT EXCEED THE STRENGTHPROPERTIES OF THE MATERIAL.

    TECHNIQUES:

    Strain gauges

    Brittle coatings analysis

    Holography

    2D , 3D photoanalysis

    Finite element analysis

    For inlays, crowns, dentures (fixed /partial/

    complete) endodontic posts and implants

    11SUMMARY

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    PHYSICAL AND MECHANICAL PROPERTIES OFDENTAL MATERIALS SHOULD WITHSTAND

    THE STRESSES OF MASTICATION

    APPLIANCES SHOULD BE DESIGNED SOTHAT THE RESULTING FORCES OF

    MASTICATION ARE DISTRIBUTED ASUNIFORMLY AS POSSIBLE

    THREE INTERRELATED FACTORS FOR LONG TERM FUNTION OF DENTAL MATERIALS ARE

    1.MATERIAL CHOICE

    2.COMPONENT GEOMETRY (to minimizestress concentration )

    3.COMPONENT DESIGN (to distribute

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    REFERENCES

    CRAIGs restorative dental materials12th & 13th ed.

    PHILLIPs science of dental materials

    11th ed.JOHN F. McCABE ,ANGUS W.G. WALLS :

    Applied dental materials. 8th ed.

    JOHN J MANAPPALLIL basic dental materials2nd ed.

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