HOA1&2 - Module 3 - PREHISTORCI ARCHITECTURE OF KERALA.pptx
2016 befib pp_textiles_final_a
1. Mechanical Properties Of Unidirectional Polypropylene
Fiber Cement Composites
Vikram Dey, Jacob Bauchmoyer, Himai Mehere, Emmanuel
Attiogbe*, Barzin Mobasher
School of Sustainable Engineering and the Built Environment
Arizona State University , Tempe, AZ 85287-5306
*Senior Expert, Development Head, Innovation Cluster Technologies, BASF
BEFIB 2016, 9th Rilem International Symposium on Fiber Reinforced Concrete,
September, 2016, Vancouver, Canada
2. Introduction
Limited Tensile applications due to
the inherent brittleness and low
tensile strength.
TRC, UHPC, SHCC class of
materials are developed
Tensile and Flexural members –
Thin section applications
Modelling and design approach
based on analytical equations
Material properties are fiber and
textile dependent
4. Development of Structural Shapes using Pulltrusion
automated pultrusion system, full
scale structural shapes composed
of TRC laminates can be
manufactured efficiently and
effectively.
Pultrusion Process Schematic Diagram
Light gage steel sections
5. Pultruded Full Size TRC Structural Shapes
Cross section of pultruded shapes with TRC laminates
6. Research Objectives
Mechanical properties and reinforcing efficiency of
hydrophilic PP Micro fibers and their comparison with
existing Macro fiber technology in the development of
structural members
Fiber testing under uniaxial tension and fiber-matrix pullout testing
Study effect of volume fraction, fiber type, matrix design
Uniaxial tension and flexural tests
Laminate systems with continuous fibers and woven textiles
developed
Digital Image Correlation (DIC) technique to quantify crack
propagation and strain localizations.
7. Filament Winding Continuous manufacturing at ASU
Hardware consists of:
National Instruments (NI) integrated system
Gearbox
Power Supply units
4-axis stepper motion controller
4-axis motion interface
NI Motion driver software
Controlled casting process
Impregnation
Chamber
Laminate Mold
Motion Controller
Wetting Tank(a)
Direction of
Fiber
Linear Guide
Stepper Motor #1
Power Supply Units
Stepper Motor #2
with gear box
Chain and Sprocket
Assembly
Fiber
Roving
Feed
Section
Guidance
Take-up
Section
Mechanical Components
10. Effect of Fiber Embedded Length Macro PP vs. Steel
Pullout energy as the area
enclosed by load slip response.
maximum for embedded length of
25 mm for all fiber types
Maximum pullout force for MAC is
similar for embedded length 20
and 25 mm. But about 40 % less
at 10 mm.
11. Specimen Groups with Continuous Fibers
Volume fraction of yarns controlled by the number of windings per length on
the mold
Mix proportions by weight: FA/C = 0.15, S/CS = 0.45,
Both direct tension and four-point flexure groups indicated by asterisks (*)
Minimum four replicate samples per group
Group
ID
Yarn
Type
Yarn
Vf
Matrix Composition
I
MAC
2200C
B
1.0%
Base Mix/ControlII* 2.5%
4.0%
IV+
MF 40
1%
Base Mix/ControlV*+ 2.5%
4.0%
Material weight (g)
Portland Cement (Type
III/IV), C
5000
Fly Ash (Class F), FA 750
Fine Silica Sand, S 2500
Water, W 2010
12. Uniaxial Tension
Closed loop servohydraulic testing
Tension specimens cut form plates with nominal dimensions: 300 x 60x 12 mm
Loading fixture clamped grips with aluminum end plates, gage length: 200 mm
Two LVDTs used to measure axial deformation
Digital image correlation technique, post-processing of images
Load Cell
LVDTs
Tension
Specimen
Hydraulic
Grip
13. Typical Tensile Response and Parameters
Elastic modulus, E1
BOP+,BOP- in the linear portion
Modulus between BOP- and BOP+ (first crack) post-BOP modulus, E2
Modulus between BOP+ and UTS, tangent modulus, E3
Actuator stroke used to calculate toughness at 2.5 % (T1), 5 % (T2) strain.
m,cr
m,cr
Elastic Modulus
of Matrix
Multiple
Cracking
Debonding
& SlipFirst
crack
A
C
D
Stage 1
Stage 2
Stage 3
Stage 4
Stress
Strain
B
(a) Tensile stress-strain evolution
BOP
BOP
14. Flexural Test
Specimens 300(L) x 62(B) x 13 (T) mm
Four point bending, span of 250 mm
Two LVDTs measured midspan deflection
Static cameras capturing images for DIC
15. Displacements in Tension and Flexure:
Stroke and LVDT
Average LVDT deformation is used for stiffness, elastic and tangent modulus
Actuator displacement is used to calculate toughness at different levels of strain.
16. Effect of curing age and dosage, MF series
MF 40 at dosages of 1.0 and
2.5% tested after 7 and 28 days
of moist curing (73 F, 90% RH)
First crack and ultimate strength
(UTS) increased marginally with
longer hydration periods
Toughness increased
considerably due to fiber content
17. Effect of Fiber Volume Fraction on Tensile
Response of MAC
Fiber reinforcement increased the
toughness
Improvement in strength and toughness
can be seen with increase in volume
fraction.
First cracking strength increases by
30% and post-crack (tangent) modulus
increases by over 107%.
The ultimate tensile strength (UTS) and
toughness measured from the area
enclosed within the stress-strain curve
increases by a factor of 2 at 4% dosage
Strengthening mechanisms - distributed
parallel cracking, crack bridging and
deflection, fiber pullout, fiber failure.
18. Effect of Fiber Dosage on Tensile Response
MF 40 vs. MAC – Significantly higher improvement in strength and toughness
with increase in volume fraction from 1.0 – 2.5%
Possible mechanisms, better bond with the matrix due to matrix penetration
between the filaments.
19. Micro Toughening Mechanism
1
2
3
Crac k Deflec tion
Debonding
Fric tional Sliding
Fibers and fiber-matrix interface prevents complete
localized failure in the matrix place through a series of
distributed cracks transverse to the direction of the load.
Distributed cracks enable deflection of matrix cracks
through fiber-matrix debonding and frictional
sliding of the fibers under tension
20. Toughening Mechanisms – MAC
Fiber bridging across loading directionDistributed cracks across loading direction
21. Toughening Mechanisms – MF 40
Cracks through thickness
Distributed cracks across
loading direction Major and minor cracks across loading direction
23. Digital Image Correlation (DIC)
Area of interest (AOI) and
subset in a reference image
Schematic presentation of a reference
subset before and after deformation
Displacements at each point of the virtual grid to obtain full-field deformation.
Automated determination of crack density, crack spacing, and damage evolution.
24. Digital Image Correlation (DIC) Technique
Evolution of distributed cracking mechanism and local 3D strain field of
filament wound composite with MAC at 4% dosage in tension.
25. DIC , MAC Vf = 4%
Displacement contour
along the gage length for
4% Vf of MAC .
Displacement distribution across
different cracks along the gage length.
Time history of stress and
crack width development
Discontinuous distribution of the longitudinal displacement can be used to measure
the crack spacing and correlated with experimental stress and strain measured locally
with transducers.
Since the onset of first crack, a general decrease in crack spacing is observed until
they reach a steady state defined as saturation crack spacing.
27. Correlation of Damage Evolution
stages of composite stress
strain where the linear
elastic stage is represented
by almost vertical line.
Various cracking stages
within the range of 1%
strain.
New cracks formation while
older cracks widen.
Pronounced strain
hardening effect is observed
as the tensile stress
increases with a reduced
stiffness.
28. MAC, Vf = 4% MF40 , Vf = 4%
Crack Spacing Distribution for MAC and MF40
29. Conclusions
Continuous Fiber reinforced concrete (FRC) is used as a base
material for TRC development
Both macro and micro PP fibers are applicable for manufacturing
continuous fiber composites
Characterization of Strain hardening behavior using Tension and
Flexural tests
– Strain softening
Distributed cracking phase and post crack stiffness is a function fiber
content
suitable for to be used thin slab applications because
Constitutive models are applicable for design procedures are based
on the ultimate strength and servicability design concept.
