Shukur Hj. Abu Hassan Dr. Yob Saed Ismail Dr. Abd. Rahman ... · PDF fileUltimate tensile...
Transcript of Shukur Hj. Abu Hassan Dr. Yob Saed Ismail Dr. Abd. Rahman ... · PDF fileUltimate tensile...
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TESTING OF COMPOSITE
MATERIALS/STRUCTURES
Shukur Hj. Abu Hassan
Dr. Yob Saed Ismail
Dr. Abd. Rahman Mohd Sam
Pusat Komposit UTM
18-19 Feb. 2003
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Designing FRP as Structural Member
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INTRODUCTION TO COMPOSITE TESTING
MECHANICAL PROPERTIES
TENSILE
COMPRESSION
SHEAR
FLEXURAL
BONDED AND BOLTED JOINTS STRENGTH
IMPACT
TEST PLANNING
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THE HISTORY
Initially used metals Test Methods
Homogenous
Isotropic
Composites require special consideration
- Nonhomogenous (Layered)
- Anisotropic (typically Orthotropic)
Early composites development limited to
Aerospace Companies
Each company developed its own procedures
Testing further complicated by continually
emerging new materials
Glass
Carbon
Aramid (Kevlar)
Boron
Epoxies etc.
General standards for testing composite
materials still do not exist.
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PROBLEMS WITH COMPOSITES
Influences of material Orthotropy – more
properties required than isotropic
materials
Laminated construction
Unidirectional composites are extremely
strong and stiff in one principal direction
and weak and flexible in the other
Temperature and moisture dependent
properties
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THE IMPORTANTS OF MECHANICAL TESTS
QUALITY CONTROL
QUALITY ASSURANCE
COMPARISONS BETWEEN MATERIALS & SELECTION
DESIGN CALCULATIONS
PREDICTION OF PERFORMANCE UNDER CONDITIONS OTHER
THAN THOSE OF THE TEST
INDICATORS IN MATERIALS DEVELOPMENT PROGRAMMES
STARTING POINTS IN THE FORMULATION OF THEORIES
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Preliminary Testing Recommended Prior to Large
Test Programme
Vendor Data
Screening Tests
Preliminary Design Data
Final Design Data
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Lamina and Laminate
Data
Typical Procedure
Characterize lamina properties first
Use Classical Lamination Theory to
Predict Laminate Properties and
Behaviour
Perform limited laminate tests to
verify theoretical predictions
Perform tensile, shear, impact,
bonding etc.
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TESTING
PROGRAMME
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Topics to be Covered For
Each Test Method
ASTM or applicable
Test Methods
Specimen geometry
Fibre orientation
Grips and Fixtures
required
Instrumentation
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Mechanical Properties
Tensile
Compression
Shear
Flexural
Bonded &
Bolted Joints
Impact
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Tensile Test
AXIAL TENSION
Axial tensile testing of unidirectional composites is a challenge
Difficult to transmit load from testing machine to the composite
Interlaminar shear strength is much lower than uniaxial tensile
strength
Shear failure in the gripping region is a common problem
Glass/epoxy or aluminium tabs are usually bonded to each end of
straight-sided specimens
Distributes gripping forces
Protects composite from surface damage
Use large bond area to minimize shear stresses
The thinner the specimen, the better
Dog bone shaped specimens are not recommended
TRANSVERSE TENSION
Transverse tensile testing is not difficult
Care is required to protect breakage due to handling use thick
specimens
Tabs not usually required
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TENSILE TESTING – RECTANGULAR COUPONS
Specifications:
ASTM D3039
ISO 527-5:1997
ISO 527-4:1997
Geometry:
250 mm x 25.4 mm (most common geometry)
Fibre Orientation:
Unidirectional, Off-axis, Crossply, Quasi-isotropic,
etc
Instrumentation:
Extensometer or strain gauges (needed to monitor
strain)
Biaxial strain gauges required for Poisson’s ratio
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Specimen Geometry (ASTM D3039
Rectangular Coupons)
Fibre orientation Recommended Specimen
Width, w
Gauge length, GL
0º (angle) 12.7 mm 138 mm
90º (angle) 25.4 mm 125 mm
0/90º (angle)
Balanced crossply25.4 mm 138 mm
GL
w
t
TL
TL – end tab length
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Specimen Geometry (ASTM D3039 Rectangular Coupons)
12
Load direction
Strain gauges (back to
back)
Overall length
w
TL
t
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TENSILE PROPERTIES
Evaluation of E11
, υ12
and σult
in longitudinal
direction.
σ1
ε1
E11 (slope)
υ12 = -(ε2/ε1) σult = Pmax/(wt)
2
1
ε1
ε2
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Tensile Test on CFRP Pultruded Plate
Specimen geometry 15mm x 228mm x 1.2mm
Ultimate tensile load = 55 kN
Ultimate tensile strength = 2700 MPa
Ultimate tensile strain = 1.8 %
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COMPRESSION TESTING
Test set up must be designed to Preclude Buckling
Test methods:
IITRI (Illinois Institute of Technology Research Institute)
ASTM D695
Geometry:
152.4 mm (length) x 25.4 mm (width)
Max. width (38.1 mm)
Thickness range 3.048 mm to 6.35 mm
Fibre orientation:
Unidirectional (0º or 90º), Cross ply (0º,90º), Quasi-isotropic, etc.
Grips and Fixtures:
IITRI Compression Test Fixture required
Instrumentation:
Back to back strain gauges recommended to monitor potential
bending during test.
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COMPRESSION TESTING
Longitudinal Compression Strength, FCL = P/wt
Compression Modulus, EC = secant modulus at –0.25%
strain due to nonlinear stress-strain curve.
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SHEAR TESTING
Various Methods Available
+/- 45º Tensile coupon
Iosipescu
Rail Shear
Interlaminar (Short Beam Shear)
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Shear Testing +/- 45 Tensile Coupons
Specification:
ASTM D3518
Geometry
250 mm x 25.4 mm (most common)
Fibre orientation:
+/- 45 lay-up only
Grips and Fixtures:
Mechanical or Hydraulic wedge grips required
Instrumentation:
Biaxial strain gauges required if shear modulus and shear strain are
desired
Very similar to rectangular tensile specimen testing
Test method only provide lamina properties
τ12, γ12 and G12
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10.0” (250 mm)
W = 1.0”
(25.4 mm)
3.0”
(76.2 mm)
0°90°
2
Glassfibre/Epoxy or
Aluminium/Epoxy
~ .060 int
1
+ 45°
P
LOADING
DIRECTION
P
+/- 45º fibre
direction
- 45º
x-x
y-y
SHEAR TEST SPECIMEN
GEOMETRY
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SHEAR PROPERTIES
Shear stress, τ12 = +/- σxx /2
Shear strain, γ 12 = εxx– εyy
In Plane Shear Modulus, G12 = σxx / 2(εxx– εyy)
In Plane Shear Strength, S12 = P max/(2wt)
τ12
γ 12
G12 (slope)
0.1% - 0.5%
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FLEXURAL TESTING
SPECIFICATION :
ASTM D790
GEOMETRY :
Length Dependent on Thickness
Span to Thickness Ratio of 16 to 1 is Recommended if Ratio of
Tensile Strength to Shear Strength is Less Than 8 to 1.
Span to Thickness Must Be Increased if Tensile Strength to Shear
Strength >8.
FIBER ORIENTATION :
Essentially Any Orientation Can Be Tested
GRIPS AND FIXTURES :
Three and/or Four Point Flexure Fixture With Variable Span Setting
Required (3 Point Most Common).
INSTRUMENTATION :
Deflectometer Required if Accurate Measurement of Mid Span
Only Load Versus Machine Crosshead Travel Recorded for Most 3-
Point Flexure Tests
Flexural strength determined by this method cannot be used for
design data
Data typically used for :
Quality control
Process verification testing
Specification purposes
Comparative type testing
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Support Span
(B)
(A)
22
LL
FLEXURAL SPECIMEN TEST SETUP
3 POINT LOADINGP
P
t
Composite reinforcement Alignment
fibre to the
beam axis
L/t
UD Carbon fibre 0º 40/1
UD Carbon fibre 90º 25/1
0º/90º Carbon fibre 0º/90º 25/1
UD Glass fibre 0º 20/1
UD Glass fibre 90º 20/1
0º/90º Glass fibre 0º/90º 20/1
0º/90º Aramid fibre 0º/90º 16/1
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Flexural Properties
Flexural Strength is given by:
fF = 1.5PL/wt2
Flexural Modulus is given by:
EF = L3m/4t3
w – specimen width, mm
P – load at failure, N
L – span between supports, mm
m – slope of linear load/deflection graph (N/mm)
t – specimen thickness, mm
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BOLT BEARING TESTING
Two most common test:
Double shear (Pin Bearing) and Single Shear
Specifications:
ASTM D953 “Bearing Strength of Plastics”
Geometry:
152.4 mm x 6 times Bolt Diameter Width (not ASTM)
6.35 mm Diameter Hole Most Common
Fibre Orientation:
Quasi-Isotropic or other Layups representative of actual
structure
Grips and Fixtures:
Mechanical or hydraulic wedges grips required
Bearing loading fixture and bolt required
Instrumentation:
No special instruments required
Load versus head deflection typically recorded.
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Double Shear (Pin Bearing) Test Configuration
152.4 mm
e=3D
6D
Bolt hole dia. = D
FBR = P/Dt
Where,
P = Failure load, N
D = Bolt diameter, mm
t= specimen thickness
FBR = bearing stress, N/mm2
t
P
Bolt
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Bolt Bearing Test
CFRP Plate
Bolted Both End
Failure load, Ff = 45 kN
Failure mode = CFRP shear out
Bolt dia. = 10 mm
Mild steel plate thickness = 2 mm
bonded to CFRP Plate
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MODES OF FAILURE FOR BOLTED JOINTS
Tension Failure
Bearing Failure
Shear out
Failure
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Shear out Failure of CFRP Plate
Shear out type failure of
CFRP Plate
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ADHESIVELY BONDED JOINT TESTING
Single Lap Shear
Double Lap Joint
Bond stress, τB = P/ (w x LB)
w
LB
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CFRP/CONCRETE PULL OUT BOND TEST
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CFRP/CONCRETE PULL OUT BOND TEST
Local shear stress distribution (Pa) versus Distance from free edge A (mm)
0
1,000,000
2,000,000
3,000,000
4,000,000
5,000,000
6,000,000
7,000,000
8,000,000
0 20 40 60 80 100 120 140
Distance from free edge (mm)
Lo
cal s
he
ar
str
es
s d
istr
ibu
tio
n (
Pa)
10 kN 20 kN 30 kN 40 kN 50 kN
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CFRP/CONCRETE PULL OUT BOND TEST
Local load at CFRP plate (N) versus Distance from free edge (mm)
-5,000
0
5,000
10,000
15,000
20,000
25,000
0 20 40 60 80 100 120 140 160
Distance from free edge (mm)
Lo
cal lo
ad
at
CFR
P p
late
(N
)
2 kN
6 kN
10 kN
16 kN
20 kN
30 kN
40 kN
50 kN
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IMPACT TESTING
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IMPACT TEST
IMPACT PROPERTIES
The impact properties of a material represent its capacity to
absorb and dissipate energies under impact shock loading such as
dropping of a hand tools and high speed collisions.
TEST STANDARD
Charpy Test Method – ISO 180/ASTM D-256
Izod Test Method – ISO 179/ASTM D-6110
Drop Weight Impact Test
The results of impact tests do not produce basic material
property data that can be used for any design purposes. The results
are useful in investigating the failure modes, energy absorption
capabilities and also in the areas of quality control & materials
development programme.
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IMPACT TEST METOHDS
95.3 mm
Striking
Pendulum
Specimen support
Charpy impact test
22 mm
Striking
Pendulum
Izod impact test
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IMPACT TEST METOHDS
Specimen support
h
Striking
Pendulum
Drop weight impact test
Position 1
Position 2Energy absorbed by specimen is
U = ½ m (v12 – v2
2) Joule
Where:
m = mass of the striking head, kg
v1 = velocity of mass just before
impact, m/s (v1 = 2gh)
v2 = velocity of mass just after
impact, m/s
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NDT RESULT ON CFRP PLATE UNDER IMPACT LOAD
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TEST PLAN
Develop Test Matrix to Identify
size, type, number of specimens,
and total amount of material
required (number of panels)
Panel fabrication Prepare work request
for NDI Perform NDIIs Panel of
Acceptable
Quality?
Prepare work request for
machining and deliver
panel to lab
Prepare test request
Deliver test request and
specimens to appropriate
Test Lab
Lab Perform Testing
Receive raw
data and
failed
specimens
from Lab
Reduce
data,
evaluate
failure
modes, etc.
Summarize data and
document in Tech Note
No
Yes
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NDI ON TEST SAMPLE
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NDI ON TEST SAMPLE
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TEST SAMPLE PREPARATION
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TEST SAMPLE PREPARATION
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STRAIN GAUGE
INSTALLATIONS
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Tensile Test on CFRP Pultruded Plate
Specimen geometry 15mm x 228mm x 1.2mm
Ultimate tensile load = 55 kN
Ultimate tensile strength = 2700 MPa
Ultimate tensile strain = 1.8 %
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Stress-strain Curve for Pultruded CFRP Plate
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Poisson Ratio
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Mode of Failure - CFRP Pultruded
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DEMO – TESTING 1
TENSILE TEST ON CFRP
SAMPLES
Location: Makmal Struktur dan
Bahan, Fakulti Kejuruteraan
Mekanikal, UTM
Person In-Charge: Shukur Hj.
Abu Hassan/Dr. Amran Alias
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DEMO – TESTING 2
FLEXURAL TEST ON
TIMBER BEAM
STRENGTHENED WITH
CFRP SHEET
Location: Makmal Struktur
dan Bahan Fakulti
Kejuruteraan Awam, UTM
Person In-Charge: Dr.
Abd. Rahman Mohd
Sam (FKA)
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DEMO – TESTING 3
1. Determination Degree of Cure of Polymer Composite using Diferrential
Scanning Calorimetry (DSC)
2. Weathering Test on FRP
3. Chemical Resistance Test on FRP
Location: Makmal Pemprosesan Polimer Fakulti Kejuruteraan Kimia &
Kejuruteraan Sumber Asli, N14, UTM
Person In-Charge: Dr. Abdul Razak Rahmat (FKKKSA)