International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1438
EXPERIMENTAL INVESTIGATION ON THE MECHANICAL PROPERTIES OF
A PMC AND HYBRID PMC
T. Santosh Kumar1, P. Lakshmi Prasanna2, A. Siva Bhaskar3
1,2B.Tech Student, Dept. of Mechanical Engineering, Gudlavalleru Engineering College, Andhra Pradesh, India
3Assistant Professor, Dept. of Mechanical Engineering, Gudlavalleru Engineering College, Andhra Pradesh, India
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - In this experimental work, the mechanical
properties of a Glass FiberReinforcedcompositearecompared
with Hybrid composite laminate reinforcedwithstainlesssteel
wire mesh is investigated. The stainless steel wire mesh along
with Glass fiber is sequentially stacked to fabricate hybrid
composite material. The laminates are fabricated using the
hand-layup method with a 50 % weight fractions of epoxy
resin, 50 % weight fractions of glass fiber and the remain
being SSWM and with a 40% weight fractions of epoxy resin,
60% of glass fiber, SSWM,. The mechanical characteristics of
the composites are obtained using tensile and drop weight
impact tests and results were compared with the theoretical
calculations.
Key Words: Glass fibre, Hybrid composite, hand layup
process, laminate, SSWM.
1. INTRODUCTION
Polymer-matrix composites consist of a polymerresinas
the matrix, with fibers as the reinforcement medium. These
materials are used in the greatest diversity of composite
applications, as well as in the largest quantities, in light of
their room-temperature properties ease of fabrication, and
cost. Hybrid Composite: A relatively new fiber-reinforced
composite is the hybrid, which is obtained by using two or
more different kinds of fibers in a single matrix; hybrids
have a better all-around combination of properties than
composites containing only a single fiber type. A variety of
fiber combinations and matrix materials are used.
2. FABRICATION OF COMPOSITE
The laminates are fabricated using the hand-layup
method. The processing steps are quite simple. First of all, a
release gel is sprayed on the mold surface to avoid the
sticking of polymer to the surface. Thin plastic sheets are
used at the top and bottom of the mold plate to get good
surface finish of the product. Reinforcement in the form of
mesh or strand mats are cut as per the mold size and placed
at the surface of mold. Then thermosetting polymer in liquid
form is mixed thoroughly in suitable proportion with a
prescribed hardener and poured onto the surface of mesh
already placed in the mold. The polymer is uniformly spread
with the help of brush. Second layer of mat is then placed on
the polymer surface and a roller is moved with a mild
pressureon the mat-polymerlayertoremoveanyairtrapped
as well as the excess polymer present. In present work the
resin LY556 with hardener is selected as polymer and Glass
Fibers for composite sheet, glass fiber and Stainless Steel
wire mesh for hybrid composite. The following Laminates
were made using Hand Lay-Up method.
Resin + Glass Fiber (PMC) .
Resin + Glass Fiber + Stainless Steel Wire Mesh (HPMC).
3. Test Specimen Preparation
Consider the typical tensile specimen shown in Fig. 1. It
has enlarged ends or shoulders for gripping. The important
part of the specimen is the gage section. The cross-sectional
area of the gage section is reduced relative to that of the
remainder of the specimen so that deformation and failure
will be localized in this region. The gage length is the region
over which measurements are made and is centered within
the reduced section. The distances between the ends of the
gage section and the shoulders should be great enough so
that the larger ends do not constrain deformation withinthe
gage section, and the gage length should be great relative to
its diameter.
Fig. 1: Tensile specimen
Izod Impact testing is an ASTM standard method of
determining the impact resistance of materials. A pivoting
arm is raised to a specific and then released. The armswings
down hitting a notched sample, breaking the specimen. The
energy absorbed by the sample is calculated from the height
the arm swings to after hitting the sample. A notchedsample
is generally used to determine impact energy and notch
sensitivity. Charpy impact testing involves striking a
standard notched specimen with a controlled weight
pendulum swung from a set height. The standard Charpy-V
notch specimen is 55mm long, 10mm square and has a 2mm
deep notch with a tip radius of 0.25mm machined on one
face.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1439
Fig 2: Izod & Charpy Test Specimen
4. EXPERIMENTAL RESULTS
The test sample is securely held by top and bottom grips
attached to the tensile or universal testing machine. During
the tension test, the grips are moved apart at a constant rate
to pull and stretch the specimen. The force on the specimen
and its displacement is continuously monitored and plotted
on a stress-strain curve until failure. The
measurements, tensile strength, yield strength and young’s
modulus, are calculated after the tensile test specimen has
broken. The tensile test and Impact testresultsaretabulated
corresponding to the two composites, PMC (Glass fiber) and
HPMC (Glass fiber + SSWM).
Table -1: Tensile Test (Glass Fiber)
Fig 3: Before Testing
Fig 4: After Testing
Table2: Tensile Test (Glass Fiber + Stainless Steel)
Fig 5: Before Testing
Fig 6: After Testing
Table3: IZOD Test (Glass Fiber)
S.No Composite
(Random
Orientation)
Ult.Load
(KN)
Disp.at
FMax
(mm)
Max.Disp
(mm)
1 Glass Fibre 10.16 4.7 5.5
2 Glass Fibre 10.78 3.4 4.0
3 Glass Fibre 11.46 5.0 5.3
Average 10.8 4.36 4.93
S.No Composite
(Random
orientation)
Area at
the Notch
(mm2)
Energy
absorbed
(J)
Impact
(J/mm2)
1 Glass Fibre 80 166 2.075
2 Glass Fibre 80 164 2.05
3 Glass Fibre 80 162 2.025
Average 164 2.05
S.No Hybrid
Composite
(Random
Orientation)
Ult.Load
(KN)
Disp.at
FMax
(mm)
Max.Disp
(mm)
1 GF+ SS 15.08 3.8 4.1
2 GF+ SS 13.46 4.4 4.6
3 GF+ SS 13.94 10.7 11.0
Average 14.16 6.3 6.56
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1440
Fig 5: Before Testing
Fig 6: Before Testing
Table 4: IZOD Test (Glass Fiber + Stainless Steel)
S.No Hybrid
Composite
(Random
orientation)
Area
at the
Notch
(mm2)
Energy
absorbed
(J)
Impact
(J/mm2)
1 Stainless
Steel
(Random
oriented)
80 286 3.575
2 Stainless
Steel
(Random
oriented)
80 288 3.6
3 Stainless
Steel
(Random
oriented)
80 290 3.625
Average 288 3.6
Fig 7: Before Testing
Fig 8: Before Testing
The test results were compared by plotting graphs
between the two composites.
Graph 1: Tensile Test
The graph trend shows that there is a decrese in the
ultimate strenghth because of introducing SSWM into Glass
fibers.
Graph 2: IZOD Test
The graph trend shows that there is a slight increment in
the impact strength because of introducing SSWM into Glass
fibers.
5. CONCLUSIONS
 From the results, the following observations and
conclusions are drawn.
 The ultimate strength and breaking load of GFRP
(random orientation) is 59.99 Gpa and Impact
strength =2.05 J/mm2.
 The ultimate strength and breaking load of Hybrid
composite is 48.66 GPA and Impact strength =2.058
J/mm2.
 The Stainless Steel Wire Mesh is completely
laminated under glass fiber, as a result the hybrid
composite material has the same brittle property at
outer layersas that of GFRP,due towhichtheductile
properties of stainless steel wire mesh has less
significance when compared to GFRP.
 The orientation of Glass fibers is random, due to
which the applied load is not completelytransferred
to SSWM. Hence the significance of load bearing
capacity of wire mesh is not appreciable. If the Glass
Fibers are laminated inpredefinedorientationsthen
there is a chance of significant improvement in the
properties can be observed in hybrid composite.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1441
6. REFERENCES
[1] Ranga Raj R., Velmurugan R., Dinesh C., Balaji S.
(Department of Aeronautical Engineering, Anna
University, Chennai)”Experimental Test of Stainless
Steel Wire Mesh and Aluminium Alloy With Glass Fiber
Reinforcement Hybrid Composite”. Int. Journal of
Engineering Research and Applications ISSN : 2248-
9622, Vol.5, Issue 5, (Part -6) May 2015, pp.80-88.
[2] C. Soutis, Carbon fibre reinforced plastics in aircraft
construction, Materials Science and Engineering, A, 412
(2005), 1–2, 171–176, doi:10.1016/j.msea.2005.08.064
[3] V. S. Sreenivasan, D. Ravindran,V. Manikandan, R.
Narayanasamy, Mechanical properties of randomly
oriented short Sansevieria cylindrica fibre/polyester
composites, Materials and Design, 32 (2011) 4, 2444–
2455, doi:10.1016/j.matdes.2010.11.042
[4] M. I. Ismail, Q. Payam Shafigh, Md. Zamin Jumaat, A.
Ibrahim Abdull, Z. Ibrahim,U. Johnson Alengaram, The
use of wire mesh–epoxy composite for enhancing the
flexural performance of concrete beams, Materials and
Design, 60 (2014) 11, 250–259,
doi:10.1016/j.matdes.2014.03.075
[5] 7 M. I. Okereke, Flexural response of polypropylene/ E-
glass fibre reinforced unidirectional composites,
Composites Part B: Engineering, 89 (2016), 388–396.
doi:10.1016/j.compositesb. 2016.01.007

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IRJET- Experimental Investigation on the Mechanical Properties of a PMC and Hybrid PMC

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1438 EXPERIMENTAL INVESTIGATION ON THE MECHANICAL PROPERTIES OF A PMC AND HYBRID PMC T. Santosh Kumar1, P. Lakshmi Prasanna2, A. Siva Bhaskar3 1,2B.Tech Student, Dept. of Mechanical Engineering, Gudlavalleru Engineering College, Andhra Pradesh, India 3Assistant Professor, Dept. of Mechanical Engineering, Gudlavalleru Engineering College, Andhra Pradesh, India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - In this experimental work, the mechanical properties of a Glass FiberReinforcedcompositearecompared with Hybrid composite laminate reinforcedwithstainlesssteel wire mesh is investigated. The stainless steel wire mesh along with Glass fiber is sequentially stacked to fabricate hybrid composite material. The laminates are fabricated using the hand-layup method with a 50 % weight fractions of epoxy resin, 50 % weight fractions of glass fiber and the remain being SSWM and with a 40% weight fractions of epoxy resin, 60% of glass fiber, SSWM,. The mechanical characteristics of the composites are obtained using tensile and drop weight impact tests and results were compared with the theoretical calculations. Key Words: Glass fibre, Hybrid composite, hand layup process, laminate, SSWM. 1. INTRODUCTION Polymer-matrix composites consist of a polymerresinas the matrix, with fibers as the reinforcement medium. These materials are used in the greatest diversity of composite applications, as well as in the largest quantities, in light of their room-temperature properties ease of fabrication, and cost. Hybrid Composite: A relatively new fiber-reinforced composite is the hybrid, which is obtained by using two or more different kinds of fibers in a single matrix; hybrids have a better all-around combination of properties than composites containing only a single fiber type. A variety of fiber combinations and matrix materials are used. 2. FABRICATION OF COMPOSITE The laminates are fabricated using the hand-layup method. The processing steps are quite simple. First of all, a release gel is sprayed on the mold surface to avoid the sticking of polymer to the surface. Thin plastic sheets are used at the top and bottom of the mold plate to get good surface finish of the product. Reinforcement in the form of mesh or strand mats are cut as per the mold size and placed at the surface of mold. Then thermosetting polymer in liquid form is mixed thoroughly in suitable proportion with a prescribed hardener and poured onto the surface of mesh already placed in the mold. The polymer is uniformly spread with the help of brush. Second layer of mat is then placed on the polymer surface and a roller is moved with a mild pressureon the mat-polymerlayertoremoveanyairtrapped as well as the excess polymer present. In present work the resin LY556 with hardener is selected as polymer and Glass Fibers for composite sheet, glass fiber and Stainless Steel wire mesh for hybrid composite. The following Laminates were made using Hand Lay-Up method. Resin + Glass Fiber (PMC) . Resin + Glass Fiber + Stainless Steel Wire Mesh (HPMC). 3. Test Specimen Preparation Consider the typical tensile specimen shown in Fig. 1. It has enlarged ends or shoulders for gripping. The important part of the specimen is the gage section. The cross-sectional area of the gage section is reduced relative to that of the remainder of the specimen so that deformation and failure will be localized in this region. The gage length is the region over which measurements are made and is centered within the reduced section. The distances between the ends of the gage section and the shoulders should be great enough so that the larger ends do not constrain deformation withinthe gage section, and the gage length should be great relative to its diameter. Fig. 1: Tensile specimen Izod Impact testing is an ASTM standard method of determining the impact resistance of materials. A pivoting arm is raised to a specific and then released. The armswings down hitting a notched sample, breaking the specimen. The energy absorbed by the sample is calculated from the height the arm swings to after hitting the sample. A notchedsample is generally used to determine impact energy and notch sensitivity. Charpy impact testing involves striking a standard notched specimen with a controlled weight pendulum swung from a set height. The standard Charpy-V notch specimen is 55mm long, 10mm square and has a 2mm deep notch with a tip radius of 0.25mm machined on one face.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1439 Fig 2: Izod & Charpy Test Specimen 4. EXPERIMENTAL RESULTS The test sample is securely held by top and bottom grips attached to the tensile or universal testing machine. During the tension test, the grips are moved apart at a constant rate to pull and stretch the specimen. The force on the specimen and its displacement is continuously monitored and plotted on a stress-strain curve until failure. The measurements, tensile strength, yield strength and young’s modulus, are calculated after the tensile test specimen has broken. The tensile test and Impact testresultsaretabulated corresponding to the two composites, PMC (Glass fiber) and HPMC (Glass fiber + SSWM). Table -1: Tensile Test (Glass Fiber) Fig 3: Before Testing Fig 4: After Testing Table2: Tensile Test (Glass Fiber + Stainless Steel) Fig 5: Before Testing Fig 6: After Testing Table3: IZOD Test (Glass Fiber) S.No Composite (Random Orientation) Ult.Load (KN) Disp.at FMax (mm) Max.Disp (mm) 1 Glass Fibre 10.16 4.7 5.5 2 Glass Fibre 10.78 3.4 4.0 3 Glass Fibre 11.46 5.0 5.3 Average 10.8 4.36 4.93 S.No Composite (Random orientation) Area at the Notch (mm2) Energy absorbed (J) Impact (J/mm2) 1 Glass Fibre 80 166 2.075 2 Glass Fibre 80 164 2.05 3 Glass Fibre 80 162 2.025 Average 164 2.05 S.No Hybrid Composite (Random Orientation) Ult.Load (KN) Disp.at FMax (mm) Max.Disp (mm) 1 GF+ SS 15.08 3.8 4.1 2 GF+ SS 13.46 4.4 4.6 3 GF+ SS 13.94 10.7 11.0 Average 14.16 6.3 6.56
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1440 Fig 5: Before Testing Fig 6: Before Testing Table 4: IZOD Test (Glass Fiber + Stainless Steel) S.No Hybrid Composite (Random orientation) Area at the Notch (mm2) Energy absorbed (J) Impact (J/mm2) 1 Stainless Steel (Random oriented) 80 286 3.575 2 Stainless Steel (Random oriented) 80 288 3.6 3 Stainless Steel (Random oriented) 80 290 3.625 Average 288 3.6 Fig 7: Before Testing Fig 8: Before Testing The test results were compared by plotting graphs between the two composites. Graph 1: Tensile Test The graph trend shows that there is a decrese in the ultimate strenghth because of introducing SSWM into Glass fibers. Graph 2: IZOD Test The graph trend shows that there is a slight increment in the impact strength because of introducing SSWM into Glass fibers. 5. CONCLUSIONS  From the results, the following observations and conclusions are drawn.  The ultimate strength and breaking load of GFRP (random orientation) is 59.99 Gpa and Impact strength =2.05 J/mm2.  The ultimate strength and breaking load of Hybrid composite is 48.66 GPA and Impact strength =2.058 J/mm2.  The Stainless Steel Wire Mesh is completely laminated under glass fiber, as a result the hybrid composite material has the same brittle property at outer layersas that of GFRP,due towhichtheductile properties of stainless steel wire mesh has less significance when compared to GFRP.  The orientation of Glass fibers is random, due to which the applied load is not completelytransferred to SSWM. Hence the significance of load bearing capacity of wire mesh is not appreciable. If the Glass Fibers are laminated inpredefinedorientationsthen there is a chance of significant improvement in the properties can be observed in hybrid composite.
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 07 | July 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1441 6. REFERENCES [1] Ranga Raj R., Velmurugan R., Dinesh C., Balaji S. (Department of Aeronautical Engineering, Anna University, Chennai)”Experimental Test of Stainless Steel Wire Mesh and Aluminium Alloy With Glass Fiber Reinforcement Hybrid Composite”. Int. Journal of Engineering Research and Applications ISSN : 2248- 9622, Vol.5, Issue 5, (Part -6) May 2015, pp.80-88. [2] C. Soutis, Carbon fibre reinforced plastics in aircraft construction, Materials Science and Engineering, A, 412 (2005), 1–2, 171–176, doi:10.1016/j.msea.2005.08.064 [3] V. S. Sreenivasan, D. Ravindran,V. Manikandan, R. Narayanasamy, Mechanical properties of randomly oriented short Sansevieria cylindrica fibre/polyester composites, Materials and Design, 32 (2011) 4, 2444– 2455, doi:10.1016/j.matdes.2010.11.042 [4] M. I. Ismail, Q. Payam Shafigh, Md. Zamin Jumaat, A. Ibrahim Abdull, Z. Ibrahim,U. Johnson Alengaram, The use of wire mesh–epoxy composite for enhancing the flexural performance of concrete beams, Materials and Design, 60 (2014) 11, 250–259, doi:10.1016/j.matdes.2014.03.075 [5] 7 M. I. Okereke, Flexural response of polypropylene/ E- glass fibre reinforced unidirectional composites, Composites Part B: Engineering, 89 (2016), 388–396. doi:10.1016/j.compositesb. 2016.01.007