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IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
__________________________________________________________________________________________________
Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 62
STUDY OF EFFECT OF COOLING RATE ON MECHANICAL AND
TRIBOLOGICAL PROPERTIES OF CAST Al-6.5Cu ALUMINUM ALLOY
S.Ilangovan1
, SaiKrishna Viswanathan2
, Gopath Niranthar K3
1
Assistant Professor (SG), Department of Mechanical Engineering Amrita School of Engineering, Amrita Vishwa
Vidyapeetham Coimbatore, Tamil Nadu, India
2
Third Year B.Tech, Department of Mechanical Engineering, Amrita School of Engineering, Amrita Vishwa
Vidyapeetham Coimbatore, Tamil Nadu, India
3
Third Year B.Tech, Department of Mechanical Engineering, Amrita School of Engineering, Amrita Vishwa
Vidyapeetham Coimbatore, Tamil Nadu, India
Abstract
Solidification time is known to have a large effect on the microstructure of cast Aluminium alloys and hence its properties. This study
is conducted to quantify how the mechanical properties of Al-6.5 Cu alloy vary with respect to the solidification time. The
solidification time is varied by varying the diameter of the cast rod; this is based on the Chvorinov’s rule which gives a relation
between solidification time and surface area, volume of the specimen. Mechanical properties such as Ultimate Tensile Strength,
Micro- hardness are observed by experimentation and change in microstructure for all the different specimens are also studied and
inferred. It is observed that as the solidification time increases, the mechanical properties tend to decrease. Further the coefficient of
friction is independent of the hardness and weight loss is dependent on hardness of the alloy.
Keywords: Solidification time, Chvorinov’s rule, grain structure, hardness, Ultimate Tensile Strength.
-----------------------------------------------------------------------***----------------------------------------------------------------------
1. INTRODUCTION
The wide variety of properties (appearance, light weight,
fabricability, physical properties, mechanical properties, and
corrosion resistance) possessed by aluminium makes it an
automatic choice for several industrial applications. It is
widely used in almost all industries [1]. Since pure aluminium
has poor mechanical properties, to enhance the properties,
aluminium is generally alloyed with other metals like copper,
zinc, magnesium and manganese. Aluminium alloys have
been used as substitute materials in automobile industries.
Grey iron has been substituted by aluminium alloy for better
fuel economy [2]. Aluminium copper alloys are widely used
and have major role in aerospace and light weight applications
[1].
The ultimate physical and mechanical properties of the cast
metal will depend upon both intrinsic factors (chemical
composition, cooling rate during solidification and heat and
mechanical treatment after solidification) and extrinsic factors
(metal cleanliness, additives for microstructure control,
casting design, riser and gating design, solidification rate
control, and temperature control subsequent to solidification)
present in each casting event and in the processing events
subsequent to casting [3,4].
Out of the several methods that have been experimented to
improve the properties of Al-Cu alloys it was studied that the
rapid cooling technique increase the mechanical and
tribological properties of the alloys as desired [5].
Cooling rate can be determinant of material properties. Areas
of casting that tend to cool rapidly have better mechanical
properties as compared to the slowly cooled ones. For the ones
with rapid cooling rate, the deposition of partially soluble
compounds at the boundaries is very less; hence these areas
have better mechanical and tribological properties [6].
The microstructure and lattice structures may vary depending
on the temperature and rate at which cooling occurs. The
subtle changes produce a marked effect on the properties of
cast component [7].
Some mathematical equations have been developed to get
relationship between cooling rate and the mechanical and
tribological properties of casting [8]. One such relation is
Chvorinov’s rule. Therefore the purpose of this work is to
show the effects of cooling rate on mechanical and tribological
properties of Al-6.5Cu alloy on the basis of Chvorinov’s rule.
2. EXPERIMENTAL PROCEDURE
2.1 Melting and Alloying
Moulds of different sizes (varying diameter from 15 to 35 mm
with the increment of 5 mm and keeping the height constant as
150 mm) are made to obtain different cooling rates (based on
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
__________________________________________________________________________________________________
Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 63
Chvorinov’s rule). Commercially available aluminium
AA1100 is melted and alloyed with electrolytic pure copper in
a crucible furnace. The melt is poured into sand moulds. After
solidification the cast rod is tested for its composition using
spectroscopic analysis. Figure 1 shows the cast rods of the
alloy.Table-1 shows the composition of the cast alloy.
Fig – 1: Cast alloy rods
Table - 1: Composition of the Al-Cu alloy
Element Al Cu Fe Si Zn
Mn,
Sn, Ni
% Comp 92.2 6.52 0.52 0.519 0.114 Traces
2.2 Specimen Preparation
The sand cast alloy rods are machined to specimens for
hardness testing, microscopic examination and tensile testing.
Appropriate ASTM standards are used for the preparation of
the specimens.
2.3 Micro-Hardness
Micro-hardness of the alloy specimens are measured in HV
scale by applying a load of 100 gram force for 20 seconds
using a diamond indenter. Micro-Hardness is randomly
measured at 6 points. The average of the 6 readings is taken to
get the value of hardness of the specimen. The effect of
cooling rate on micro-hardness is inferred based on the results.
Figure 2 shows the Mitutoyo make micro-hardness tester.
Fig – 2: Micro-hardness tester
2.4 Tensile Test
Tensile test of the machined alloy is performed on a Universal
Tensile Testing Machine. The stress versus strain graph of the
specimen is plotted and the ultimate tensile strength is found
out from the plot. The effect of cooling rate on tensile strength
is inferred based on the results. Figure 3 shows the tensile
specimen of the alloy. Figure 4 shows the tensile test specimen
machined out from cast rods.
Fig – 3: Drawing of tensile specimen
Fig – 4: Photographic image of tensile test specimen
Figure 5 shows the experimental setup of the tensile test
Fig – 5: Universal testing machine
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
__________________________________________________________________________________________________
Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 64
2.5 Microstructure
Metallographic specimens are prepared using standard
grinding and polishing procedures. For microstructure
analysis, the specimen is etched with HF solution and Kellers
reagent. The effect of cooling rate on microstructure is
inferred based on the results.
2.6 Wear Test
The wear test is carried out using DUCOM make pin-on-disc
wear tester. The specimen is machined to size diameter 10 mm
and length 40 mm. The test parameters used are: Speed-236
rpm; Velocity-1 m/s; Load-20 N; Track Radius- 40 mm;
Sliding Time-10 minutes.
Fig-6: Wear and Friction monitor
3. RESULTS AND DISCUSSION
3.1 Variation in Cooling Rate
It is well known that Chvorinov’s rule gives a relation
between solidification time and surface area and volume of a
casting as defined by the following equation (1).
T = B*(V/A)n
-------------- (1)
where, B = Mould Constant
n = constant
V = Volume of casting
A = Surface Area of casting
T = Solidification time
This relationship gives the liberty to vary the diameters of the
castings (keeping height constant) to obtain different cooling
rates.
3.2 Micro-Hardness
Figure 7 is plotted between hardness value and the diameter of
the specimens. It is observed that as the diameter of the
specimen increases, the hardness value decreases. The reason
for the variation is due to the fact that as the diameter
increases, the time for solidification of the casting increases.
Further, as the diameter increases, larger grain structures are
formed due to slow cooling and hence giving a declining trend
in mechanical properties [9]. The variation of hardness value
with diameter is shown in Table 2.
Table - 2: Variation of hardness with diameter
Diameter (mm) 15 20 25 30 35
Hardness (HV) 87.4 83.9 79.6 75.8 71.6
Fig - 7: Plot of variation of micro hardness with diameter
3.3 Tensile Test
Figure 8 is plotted between ultimate tensile strength (UTS)
and diameter of the specimens. From the plot it is observed
that the UTS value decreases as the diameter increases. It is
due to lower hardness observed in the larger diameter
specimen as compared to smaller diameter. As a general rule,
UTS is function of hardness of the alloy. That is if hardness
decreases, the UTS also proportionally decreases. The nature
of fracture observed in this study is brittle fracture because of
cast specimen. Table 3 shows the UTS value of the alloy for
different diameters.
Table - 3: Variation of UTS with diameter
Diameter (mm) 15 20 25 30 35
UTS (MPa) 107 104.2 99.8 90.3 88.1
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
__________________________________________________________________________________________________
Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 65
Fig – 8: Plot of variation of UTS with diameter
3.4 Microstructure
The microstructure of the specimens of the alloy castings of
diameter 15, 25 and 35 mm (Figures 9-11) is chosen so as to
find a significant difference in grain structure. By comparing
Figures 9 and 11, it is observed that for 15 mm diameter
casting the grain size is very small as compared to 35 mm
diameter casting. This is due to the fact that for smaller
diameter, the cooling rate is very high which leads to smaller
grain size and for larger diameter it is low and forming large
grain size. Microstructure showed a marked shift from large
sized dendrites to finer dendrites this is in accordance with
previous report [10].
Fig - 9: Microstructure of 15 mm diameter casting showing
finer grains
Fig - 10: Microstructure of 25 mm diameter casting showing
bigger grains
Fig - 11: Microstructure of 35 mm diameter casting showing
relatively bigger grains than 25 mm diameter
3.5 Coefficient of Friction
Figure 12 shows the variation of coefficient of friction with
hardness of the alloy. From the figure it is observed that the
COF value is not varied significantly with hardness of the
alloy. This shows COF is independent of the hardness of the
alloy. It is in consistence with previous report [9, 11-12].
Fig-12: Plot of COF versus Hardness
3.6 Wear
The weight loss is measured by subtracting final weight from
initial weight of the specimens. It is expressed in grams.
Figure 13 is plotted between weight loss and hardness of the
alloy specimens. It is found that weight loss decreases as the
hardness increases. Hence it may be concluded that weight
loss is function of hardness of alloy.
Fig-13: Variation of weight loss with hardness
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
__________________________________________________________________________________________________
Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 66
4. CONCLUSIONS
The effect of cooling rate on mechanical properties of cast
aluminium Al-6.5Cu alloy is studied and the following
conclusions are derived.
 Hardness of the alloy decreases as the diameter of the
cast rod increases, which is due to slow cooling of the
larger diameter as compared to smaller diameter.
 Ultimate Tensile Strength decreases with increase in
diameter. The reason being, in the case of larger
diameter rod, the hardness is less.
 The size of grain structure increases with increase in
diameter which is subjected to slow cooling.
 Coefficient of Friction is independent of hardness of
the alloy.
 Weight loss is dependent on hardness of the alloy.
REFERENCES
[1] ASM Metals Handbook, “Properties and Selection of
Nonferrous Alloys and Special Purpose Materials”,
ASM International, Vol.2, pp. 17-19.
[2] Lozano DE, Mercado-solis RD, Perez AJ, Talamantes J
and Morales F (2009), “Tribological behavior of cast
hypereutectic Al-Si-Cu alloy subjected to sliding
wear”, wear, Vol 267, pp 545-549.
[3] Kalpakjian S (2008), “Manufacturing processes for
engineering materials”, Fifth Edition.
[4] Cantor B (2003), “Solidification and casting”, Series in
Materials Science and Engineering.
[5] Musa Gogebakan, Orhan Uzun, Tuncay Karaaslan and
Mustafa Keskin (2003), “Rapidly solidified Al-6.5
wt.% Ni alloy”, Journal of Materials Processing
Technology, Vol 143, pp 87-92.
[6] Dr.Eman J. Abed,” The influence of different casting
method on solidification time and mechanical
properties of AL- Sn castings”, International Journal of
Engineering & Technology IJET-IJENS, Vol 11, No:
06, pp 34-44.
[7] Mitchell RJ, Preuss M, Hardy MC and Tin S(2006),
“Influence of composition and cooling rate on
constrained and unconstrained lattice parameters in
advances polycrystalline nickel-base superalloys”,
Journal of Materials Science and Engineering A, Vol
423, pp 282-291.
[8] Savaskan T, Turhal MS (2003), “Relationships
between cooling rate, copper content and mechanical
properties of monotectoid based Zn-Al-Cu alloys ,
Materials Characterization, Vol 51, pp 259-270.
[9] Ilangovan S (2014), “Effects of Solidification time on
mechanical properties and wear behaviour of sand cast
Aluminium alloy”, International Journal of Research in
Engineering and Technology Plating and Surface
Finishing, Vol 3,Issue 2,pp 71-75.
[10] Amin KM, Nadeem A Mufti (2012), “Investigating
cooling curve profile and microstructure of a squeeze
cast Al-4%Cu alloy”, Journal of Materials Processing
Technology, Vol 212, pp 1631-1639.
[11] Ilangovan S and Sellamuthu R (2012), “An
Investigation of the effect of Ni Content and Hardness
on the wear behavior of Sand Cast Cu-Ni-Sn Alloys”,
International Journal of Microstructure and Materials
Properties, Vol 7, pp 316-328.
[12] Ilangovan S and Sellamuthu R (2013), “Effects of Tin
on Hardness, Wear Rate and Coefficient of Friction of
Cast Cu-Ni-Sn Alloys”, Journal of Engineering Science
& Technology, Vol 8, No.1, pp 44-54.
BIOGRAPHIES
Dr. S. Ilangovan has completed his
Bachelor’s Degree in Mechanical
Engineering and Master’s Degree in
Production Engineering. He has fourteen
years of experience in industry and sixteen
years in teaching. He has also completed
Ph.D. in Materials Engineering
SaiKrishna Viswanathan is a third-year
Mechanical Engineering student currently
pursuing Bachelor of Technology degree
from Amrita School of Engineering, Tamil
Nadu.
Gopath Niranthar K is a third-year
Mechanical Engineering student currently
pursuing Bachelor of Technology degree
from Amrita School of Engineering, Tamil
Nadu.

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Study of effect of cooling rate on mechanical and

  • 1. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 __________________________________________________________________________________________________ Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 62 STUDY OF EFFECT OF COOLING RATE ON MECHANICAL AND TRIBOLOGICAL PROPERTIES OF CAST Al-6.5Cu ALUMINUM ALLOY S.Ilangovan1 , SaiKrishna Viswanathan2 , Gopath Niranthar K3 1 Assistant Professor (SG), Department of Mechanical Engineering Amrita School of Engineering, Amrita Vishwa Vidyapeetham Coimbatore, Tamil Nadu, India 2 Third Year B.Tech, Department of Mechanical Engineering, Amrita School of Engineering, Amrita Vishwa Vidyapeetham Coimbatore, Tamil Nadu, India 3 Third Year B.Tech, Department of Mechanical Engineering, Amrita School of Engineering, Amrita Vishwa Vidyapeetham Coimbatore, Tamil Nadu, India Abstract Solidification time is known to have a large effect on the microstructure of cast Aluminium alloys and hence its properties. This study is conducted to quantify how the mechanical properties of Al-6.5 Cu alloy vary with respect to the solidification time. The solidification time is varied by varying the diameter of the cast rod; this is based on the Chvorinov’s rule which gives a relation between solidification time and surface area, volume of the specimen. Mechanical properties such as Ultimate Tensile Strength, Micro- hardness are observed by experimentation and change in microstructure for all the different specimens are also studied and inferred. It is observed that as the solidification time increases, the mechanical properties tend to decrease. Further the coefficient of friction is independent of the hardness and weight loss is dependent on hardness of the alloy. Keywords: Solidification time, Chvorinov’s rule, grain structure, hardness, Ultimate Tensile Strength. -----------------------------------------------------------------------***---------------------------------------------------------------------- 1. INTRODUCTION The wide variety of properties (appearance, light weight, fabricability, physical properties, mechanical properties, and corrosion resistance) possessed by aluminium makes it an automatic choice for several industrial applications. It is widely used in almost all industries [1]. Since pure aluminium has poor mechanical properties, to enhance the properties, aluminium is generally alloyed with other metals like copper, zinc, magnesium and manganese. Aluminium alloys have been used as substitute materials in automobile industries. Grey iron has been substituted by aluminium alloy for better fuel economy [2]. Aluminium copper alloys are widely used and have major role in aerospace and light weight applications [1]. The ultimate physical and mechanical properties of the cast metal will depend upon both intrinsic factors (chemical composition, cooling rate during solidification and heat and mechanical treatment after solidification) and extrinsic factors (metal cleanliness, additives for microstructure control, casting design, riser and gating design, solidification rate control, and temperature control subsequent to solidification) present in each casting event and in the processing events subsequent to casting [3,4]. Out of the several methods that have been experimented to improve the properties of Al-Cu alloys it was studied that the rapid cooling technique increase the mechanical and tribological properties of the alloys as desired [5]. Cooling rate can be determinant of material properties. Areas of casting that tend to cool rapidly have better mechanical properties as compared to the slowly cooled ones. For the ones with rapid cooling rate, the deposition of partially soluble compounds at the boundaries is very less; hence these areas have better mechanical and tribological properties [6]. The microstructure and lattice structures may vary depending on the temperature and rate at which cooling occurs. The subtle changes produce a marked effect on the properties of cast component [7]. Some mathematical equations have been developed to get relationship between cooling rate and the mechanical and tribological properties of casting [8]. One such relation is Chvorinov’s rule. Therefore the purpose of this work is to show the effects of cooling rate on mechanical and tribological properties of Al-6.5Cu alloy on the basis of Chvorinov’s rule. 2. EXPERIMENTAL PROCEDURE 2.1 Melting and Alloying Moulds of different sizes (varying diameter from 15 to 35 mm with the increment of 5 mm and keeping the height constant as 150 mm) are made to obtain different cooling rates (based on
  • 2. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 __________________________________________________________________________________________________ Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 63 Chvorinov’s rule). Commercially available aluminium AA1100 is melted and alloyed with electrolytic pure copper in a crucible furnace. The melt is poured into sand moulds. After solidification the cast rod is tested for its composition using spectroscopic analysis. Figure 1 shows the cast rods of the alloy.Table-1 shows the composition of the cast alloy. Fig – 1: Cast alloy rods Table - 1: Composition of the Al-Cu alloy Element Al Cu Fe Si Zn Mn, Sn, Ni % Comp 92.2 6.52 0.52 0.519 0.114 Traces 2.2 Specimen Preparation The sand cast alloy rods are machined to specimens for hardness testing, microscopic examination and tensile testing. Appropriate ASTM standards are used for the preparation of the specimens. 2.3 Micro-Hardness Micro-hardness of the alloy specimens are measured in HV scale by applying a load of 100 gram force for 20 seconds using a diamond indenter. Micro-Hardness is randomly measured at 6 points. The average of the 6 readings is taken to get the value of hardness of the specimen. The effect of cooling rate on micro-hardness is inferred based on the results. Figure 2 shows the Mitutoyo make micro-hardness tester. Fig – 2: Micro-hardness tester 2.4 Tensile Test Tensile test of the machined alloy is performed on a Universal Tensile Testing Machine. The stress versus strain graph of the specimen is plotted and the ultimate tensile strength is found out from the plot. The effect of cooling rate on tensile strength is inferred based on the results. Figure 3 shows the tensile specimen of the alloy. Figure 4 shows the tensile test specimen machined out from cast rods. Fig – 3: Drawing of tensile specimen Fig – 4: Photographic image of tensile test specimen Figure 5 shows the experimental setup of the tensile test Fig – 5: Universal testing machine
  • 3. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 __________________________________________________________________________________________________ Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 64 2.5 Microstructure Metallographic specimens are prepared using standard grinding and polishing procedures. For microstructure analysis, the specimen is etched with HF solution and Kellers reagent. The effect of cooling rate on microstructure is inferred based on the results. 2.6 Wear Test The wear test is carried out using DUCOM make pin-on-disc wear tester. The specimen is machined to size diameter 10 mm and length 40 mm. The test parameters used are: Speed-236 rpm; Velocity-1 m/s; Load-20 N; Track Radius- 40 mm; Sliding Time-10 minutes. Fig-6: Wear and Friction monitor 3. RESULTS AND DISCUSSION 3.1 Variation in Cooling Rate It is well known that Chvorinov’s rule gives a relation between solidification time and surface area and volume of a casting as defined by the following equation (1). T = B*(V/A)n -------------- (1) where, B = Mould Constant n = constant V = Volume of casting A = Surface Area of casting T = Solidification time This relationship gives the liberty to vary the diameters of the castings (keeping height constant) to obtain different cooling rates. 3.2 Micro-Hardness Figure 7 is plotted between hardness value and the diameter of the specimens. It is observed that as the diameter of the specimen increases, the hardness value decreases. The reason for the variation is due to the fact that as the diameter increases, the time for solidification of the casting increases. Further, as the diameter increases, larger grain structures are formed due to slow cooling and hence giving a declining trend in mechanical properties [9]. The variation of hardness value with diameter is shown in Table 2. Table - 2: Variation of hardness with diameter Diameter (mm) 15 20 25 30 35 Hardness (HV) 87.4 83.9 79.6 75.8 71.6 Fig - 7: Plot of variation of micro hardness with diameter 3.3 Tensile Test Figure 8 is plotted between ultimate tensile strength (UTS) and diameter of the specimens. From the plot it is observed that the UTS value decreases as the diameter increases. It is due to lower hardness observed in the larger diameter specimen as compared to smaller diameter. As a general rule, UTS is function of hardness of the alloy. That is if hardness decreases, the UTS also proportionally decreases. The nature of fracture observed in this study is brittle fracture because of cast specimen. Table 3 shows the UTS value of the alloy for different diameters. Table - 3: Variation of UTS with diameter Diameter (mm) 15 20 25 30 35 UTS (MPa) 107 104.2 99.8 90.3 88.1
  • 4. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 __________________________________________________________________________________________________ Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 65 Fig – 8: Plot of variation of UTS with diameter 3.4 Microstructure The microstructure of the specimens of the alloy castings of diameter 15, 25 and 35 mm (Figures 9-11) is chosen so as to find a significant difference in grain structure. By comparing Figures 9 and 11, it is observed that for 15 mm diameter casting the grain size is very small as compared to 35 mm diameter casting. This is due to the fact that for smaller diameter, the cooling rate is very high which leads to smaller grain size and for larger diameter it is low and forming large grain size. Microstructure showed a marked shift from large sized dendrites to finer dendrites this is in accordance with previous report [10]. Fig - 9: Microstructure of 15 mm diameter casting showing finer grains Fig - 10: Microstructure of 25 mm diameter casting showing bigger grains Fig - 11: Microstructure of 35 mm diameter casting showing relatively bigger grains than 25 mm diameter 3.5 Coefficient of Friction Figure 12 shows the variation of coefficient of friction with hardness of the alloy. From the figure it is observed that the COF value is not varied significantly with hardness of the alloy. This shows COF is independent of the hardness of the alloy. It is in consistence with previous report [9, 11-12]. Fig-12: Plot of COF versus Hardness 3.6 Wear The weight loss is measured by subtracting final weight from initial weight of the specimens. It is expressed in grams. Figure 13 is plotted between weight loss and hardness of the alloy specimens. It is found that weight loss decreases as the hardness increases. Hence it may be concluded that weight loss is function of hardness of alloy. Fig-13: Variation of weight loss with hardness
  • 5. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 __________________________________________________________________________________________________ Volume: 03 Issue: 05 | May-2014, Available @ http://www.ijret.org 66 4. CONCLUSIONS The effect of cooling rate on mechanical properties of cast aluminium Al-6.5Cu alloy is studied and the following conclusions are derived.  Hardness of the alloy decreases as the diameter of the cast rod increases, which is due to slow cooling of the larger diameter as compared to smaller diameter.  Ultimate Tensile Strength decreases with increase in diameter. The reason being, in the case of larger diameter rod, the hardness is less.  The size of grain structure increases with increase in diameter which is subjected to slow cooling.  Coefficient of Friction is independent of hardness of the alloy.  Weight loss is dependent on hardness of the alloy. REFERENCES [1] ASM Metals Handbook, “Properties and Selection of Nonferrous Alloys and Special Purpose Materials”, ASM International, Vol.2, pp. 17-19. [2] Lozano DE, Mercado-solis RD, Perez AJ, Talamantes J and Morales F (2009), “Tribological behavior of cast hypereutectic Al-Si-Cu alloy subjected to sliding wear”, wear, Vol 267, pp 545-549. [3] Kalpakjian S (2008), “Manufacturing processes for engineering materials”, Fifth Edition. [4] Cantor B (2003), “Solidification and casting”, Series in Materials Science and Engineering. [5] Musa Gogebakan, Orhan Uzun, Tuncay Karaaslan and Mustafa Keskin (2003), “Rapidly solidified Al-6.5 wt.% Ni alloy”, Journal of Materials Processing Technology, Vol 143, pp 87-92. [6] Dr.Eman J. Abed,” The influence of different casting method on solidification time and mechanical properties of AL- Sn castings”, International Journal of Engineering & Technology IJET-IJENS, Vol 11, No: 06, pp 34-44. [7] Mitchell RJ, Preuss M, Hardy MC and Tin S(2006), “Influence of composition and cooling rate on constrained and unconstrained lattice parameters in advances polycrystalline nickel-base superalloys”, Journal of Materials Science and Engineering A, Vol 423, pp 282-291. [8] Savaskan T, Turhal MS (2003), “Relationships between cooling rate, copper content and mechanical properties of monotectoid based Zn-Al-Cu alloys , Materials Characterization, Vol 51, pp 259-270. [9] Ilangovan S (2014), “Effects of Solidification time on mechanical properties and wear behaviour of sand cast Aluminium alloy”, International Journal of Research in Engineering and Technology Plating and Surface Finishing, Vol 3,Issue 2,pp 71-75. [10] Amin KM, Nadeem A Mufti (2012), “Investigating cooling curve profile and microstructure of a squeeze cast Al-4%Cu alloy”, Journal of Materials Processing Technology, Vol 212, pp 1631-1639. [11] Ilangovan S and Sellamuthu R (2012), “An Investigation of the effect of Ni Content and Hardness on the wear behavior of Sand Cast Cu-Ni-Sn Alloys”, International Journal of Microstructure and Materials Properties, Vol 7, pp 316-328. [12] Ilangovan S and Sellamuthu R (2013), “Effects of Tin on Hardness, Wear Rate and Coefficient of Friction of Cast Cu-Ni-Sn Alloys”, Journal of Engineering Science & Technology, Vol 8, No.1, pp 44-54. BIOGRAPHIES Dr. S. Ilangovan has completed his Bachelor’s Degree in Mechanical Engineering and Master’s Degree in Production Engineering. He has fourteen years of experience in industry and sixteen years in teaching. He has also completed Ph.D. in Materials Engineering SaiKrishna Viswanathan is a third-year Mechanical Engineering student currently pursuing Bachelor of Technology degree from Amrita School of Engineering, Tamil Nadu. Gopath Niranthar K is a third-year Mechanical Engineering student currently pursuing Bachelor of Technology degree from Amrita School of Engineering, Tamil Nadu.