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7/30/2019 Anbu Mechanical Properties of Dental Materials
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Click to edit Master subtitle style
11/12/
12
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
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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
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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
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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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