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P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35                                                                             
 

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Characterization and tensile fractography of nano ZrO2  
reinforced Copper-Zinc alloy composites 
 
 
Prasad H. Nayak 
VTU RRC, Belgaum, Dept. of Mechanical Engineering, Oxford College of Engineering, Bangalore, Karnataka, India 
Prasadnayak990@gmail.com 
 
H. K. Srinivas  
Dept. of Mechanical Engineering, SJBIT, Bangalore, Karnataka, India 
 
Madeva Nagaral 
Aircraft Research and Design Centre, Hindustan Aeronautics Limited, Bangalore, Karnataka, India 
madev.nagaral@gmail.com, http://orcid.org/0000-0002-8248-7603 
 
V. Auradi 
Dept. of Mechanical Engineering, SIT, Tumkur, Karnataka, India 
vsauradi@gmail.com 
 
 
 
ABSTRACT. Nano particulates fortified metal lattice composites are finding 
extensive variety of utilizations in car and sports hardware fabricating 
businesses. In the present investigation, an endeavor has been made to create 
copper-zinc-nano ZrO2 particulates strengthened composites by utilizing fluid 
liquefy technique. 4, 8 and 12 wt. % of nano ZrO2 particulates were added to 
the Cu-Zn base grid. Microstructural studies were finished by utilizing SEM 
and EDS examination. Mechanical behavior of Cu-Zn-4, 8, 12 wt. % of nano 
ZrO2 composites were assessed according to ASTM benchmarks. Checking 
electron micrographs uncovered the uniform dispersion of nano ZrO2 
particulates in the copper zinc composite network. EDS examination affirmed 
the nearness of Zr and O components in nano ZrO2 strengthened 
composites. Further, it was noticed that hardness, UTS, yield quality of Cu-
Zn composite expanded with the expansion of 4, 8 and 12 wt. % of nano 
ZrO2 particulates. Ductility of nano composites was decreased by adding 
zirconium oxide particulates. Fractography of tensile specimens were carried 
out by using SEM micrographs to understand the failure mechanisms. 
  
KEYWORDS. Cu-Zn Alloy; Nano ZrO2 Particulates; Liquid Melt Method; 
Mechanical Behavior; Fractography. 
 

 

 
 

Citation: Prasad, H., N., Srinivas, H, K., 
Nagaral, M., Auradi, V.,  Characterization and 
tensile fractography of nano ZrO2 reinforced 
copper zinc alloy composites, Frattura ed 
IntegritàStrutturale, 48 (2019) 370-376. 
 
Received: 17.11.2018 
Accepted: 21.01.2019 
Published: 01.04.2019 
 
Copyright: © 2019 This is an open access 
article under the terms of the CC-BY 4.0, 
which permits unrestricted use, distribution, 
and reproduction in any medium, provided 
the original author and source are credited. 

 

http://www.gruppofrattura.it/VA/48/2261.mp4


 

                                                            P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 
 

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INTRODUCTION  
 

he common name being composition material or simply a composite is combination of two or many materials 
with non-identical physical and chemical behaviors, when intermixed produces entirely different product with 
distinct characteristic when compared with the individual material characteristic. The blending of the material is 

usually done at a macroscopic level. These materials are intermixed in such a ratio that its certain properties get enhanced. 
The ratios of two materials are optimized based on their applications. These composites are used not only for their 
improvised mechanical properties, but also for thermal, electrical and environmental applications [1, 2]. These materials 
are generally preferred for different applications like concretes, reinforced plastics such as fiber reinforced polymers, metal 
composites, ceramic composites. Ceramic matrix composites & metal matrix composites are generally used for bridges 
and structure such as boat house, panels of swimming pools, bodies of sports cars, bath tubs, and storage tanks & also 
advanced materials in spacecrafts & aircrafts building which are in high demand [3, 4]. 
The composites usually consist of fiber or particulate phase which is stronger & stiffer when compared with the matrix 
phase. The fiber or particulates commonly known as reinforcement phase have good mechanical, thermal & electrical 
properties when compared to the matrix phase [5]. 
Nano Metal Matrix Composites are gradually getting to be distinctly appealing materials for cutting edge aviation 
applications and yet their properties can be custom-made by the proper chose of reinforcement. Among three different 
composites, particulate strengthened MMCs as of late discovered unique intrigue on account of their quality and firmness 
at a normal room and raised temperatures. It is important to note that the properties of the nano metal matrix are 
unequivocally affected by secondary parameters of the reinforcement, for example, shape, size, introduction, circulation 
and volume [6]. 
Among any of other commonly used metals, copper is one characterized by the best thermal conductivity and resistance 
to corrosion which explains why it is commonly chosen in the first instance for metal material. On the other hand, having 
very low mechanical properties, it must be strengthened by ceramic particles, for example, which is one of the most 
reliable methods of reinforcement. Copper based metal lattice composites (CMCs) have discovered more prominent 
applications in the field of car, air ships and machine apparatus enterprises attributable to their low thickness and 
associative high wear opposition, quality, consumption obstruction, firmness and warm conductivity. Copper and its 
combination are to a great extent utilized as a material for heading [7, 8].  
Since copper-based materials have a relativity high temperature and low wear obstruction, the copper network has been 
effectively fortified with nano zirconium oxide and graphite particles, proceeds or irregular strands, called metal matrix 
composite (MMCs).  
There is a globally developing attention in assembling clay particulate fortified metal grid materials which forms joined 
properties of its fortifications and display enhanced physical and tribo-mechanical properties.  
In the present investigation, copper-10%Zn amalgam-based composites were manufactured by stir process. Nano ZrO2 
particulates were utilized as the support. The 4, 8 and 12 wt. level of earthenware production fortifications were taken to 
create the copper-ZrO2 composites. The composites were tried for mechanical properties like hardness, extreme rigidity, 
yield quality and rate stretching according to ASTM guidelines. 

 
Elements Content wt. % 

Cu 89.20 
Zn 9.90 

Others 0.90
 

Table1: The chemical composition of Cu-Zn alloy 
 
 
EXPERIMENTAL DETAILS 

 
he Copper-Zn-nano ZrO2 composites created in this investigation contains 4, 8 and 12 wt. % of artistic nano 
ZrO2 particulates. The density of copper-zinc compound is 8.737 g/cm3 and that of ZrO2 is 5.68 g/cm3. The 
density of composites diminishes with expansion of nano ZrO2 particulates. The concoction creation of copper-

zinc combination is appeared in the Tab. 1. 
The fabrication of copper-zinc-ZrO2 composites was carried out by liquid metallurgy route via stir casting technique. The 
preparation of copper-zinc-nano ZrO2 composites was accomplished by two-stage stir casting technique. Pre-calculated 

T 

T 



 

P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35                                                                             
 

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quantity of Cu-Zn alloy ingots were charged into the heating furnace to liquefy. Though the Cu-Zn alloy melts at 1080˚C, 
the melting furnace was superheated to a temperature of 1150˚C. Thermocouples were used to measure temperature. The 
melt metal in crucible was then degassed to remove unwanted byproducts using a chemical called hexa-chloro-ethane 
(C2Cl6) upto 3 mins. A steel impeller used was coated with a ceramic material known as zirconium which is used to agitate 
by rotating the molten metal such that the vortex is created. The process of stirring was carried out at a speed of 300 rpm 
& the impeller was immersed for about 60% height of molten metal from the top surface of melt within the crucible. 
Simultaneously during the process of stirring the pre-calculated amount of reinforcement was added into the vortex in 
two-stages, to ensure good wet-ability stirring was continued for upto 5 mins. The reinforcing materials ZrO2 was 
preheated upto 500˚C in oven to remove moisture content before adding it into molten metal vortex. Now, Cu-Zn alloy 
along with 4 wt. % ZrO2 particulates were poured into solid cast iron mould to get a composite after solidification. 
Similarly, Cu-Zn-8 and 12 wt. % of ZrO2 composites were fabricated for the further studies. 
The microstructural analysis completed by utilizing SEM instrument. Tests around 5 mm thickness across taken from the 
casting samples and were cleaned appropriately. A reagent named Keller's was utilized to etch the examples. Hardness of 
as cast copper-zinc-ZrO2 amalgam composites were coordinated to know the influence of nano scale ZrO2 particles in the 
system material ASTM E 10 standard [11]. The cleaned precedents were striven for their hardness, using Brinell hardness 
testing machine, which is having a ball indenter and applying a load of 250 kg and tolerate time of 30 seconds, three 
courses of action of readings were noted at better places of the sample and an average of all the value was used for 
figuring. 
The tensile properties of the prepared samples are established as per the ASTM E8 method upon tension test piece of 
gauge-diameter 9mm with gauge-length of 45mm. Metal & its alloys are to be designed to provide material properties 
tailored to applications. Universal testing machine (UTM) is used to conduct tensile test to find out the effect of nano 
ZrO2 particulates on tensile behavior of Cu-Zn alloy composites. 
 
 
RESULTS AND DISCUSSION 
 
Microstructural Analysis 

ig. 1(a) shows microstructure of as cast copper-10% zinc alloy, fig. 1b represents Cu-Zn-12 wt.% of nano ZrO2 
composites. The SEM micrographs reveal almost uniform distribution of ZrO2 particulates throughout the matrix 
as observed in the fig. 1b. Uniformly distributed particulates increase the overall strength and other properties 

reducing the porosity of the MMC. 
Fig. 2 is the EDS spectrum of copper-zinc and 12 wt.% of nano ZrO2 reinforced composites. EDS spectrum revealed the 
presence of nano ZrO2 particles in the copper-zinc alloy matrix in the form of Zr and O elements along with Cu and Zn 
matrix elements. 
 

                                        
                                                        (a)                                                                                   (b) 

Figure 1: SEM micrographs of (a) as cast copper-zinc alloy (b) copper-12 wt. % ZrO2 composite 

F 



 

                                                            P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 
 

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Figure 2: EDS spectrum of copper-zinc-12 wt. % ZrO2 composite 
 
 
HARDNESS MEASUREMENTS 
 

ardness is a property of a material that demonstrates the capacity of the material to oppose nearby plastic 
disfigurement. Fig. 3 demonstrates the impact of the nano ZrO2 molecule substance on the hardness of the 
copper-zinc compound. The hardness esteems are decidedly related with the weight level of nano particles, since 

particles fortified the lattice. Moreover, the outcomes demonstrate that nano particles fortified MMCs harder than copper-
zinc composite because of Hall-Petch and Orowan fortifying components and in addition the great interface between the 
fortification and framework. Copper-zinc and 12 wt. % nano ZrO2 composites demonstrate more hardness; the expansion 
in hardness of these composites can be ascribed to the scattering fortifying impact [13]. By including 12 wt. % nano ZrO2 
particulates into the copper combination, the hardness of copper amalgam expanded to 85.4 BHN from 126.7 BHN. 
 

 
Figure 3: Showing the hardness of as cast copper-zinc alloy and nano ZrO2 composites 

 
 

TENSILE BEHAVIOR 
 

ig. 4 and 5 demonstrating the tensile properties of copper-zinc combination and copper-zinc-4, 8 and 12 wt. % 
nano ZrO2 composite. Fig. 4 demonstrating the ultimate strength (UTS) of copper-10% zinc compound and ZrO2 
composites. Fig. 4 it is apparent that UTS of copper-zinc-ZrO2 composite is much more than the base lattice 

H 

F 



 

P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35                                                                             
 

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combination. By including 3, 8 and 12 wt. % of nano ZrO2 nano particulates to the base amalgam UTS has expanded 
from 329.7 MPa to 435 MPa. From the fig. 4 it was discovered that yield quality of the copper-zinc base compound is 
275.6 MPa and in copper-zinc-12 wt. % nano ZrO2 composite is 356.2 MPa. It demonstrated a change of 29 % in yield 
quality. 
The expansion in UTS and YS is essentially because of solid holding between fortification particles and copper-zinc grid, 
plays an imperative role on the load exchanging from network to support. This is a result of grain refinement and 
molecule fortifying [14, 15]. The upgrades of quality are influenced by the higher load bearing and confound fortifying 
caused by nano ZrO2 particles. In contrast with the base copper, the immense improvement in the quality saw in the 
composites is because of the nearness of the particles as obstructions that confine the movement of separations caught by 
ZrO2 particulates. This will prompt increment the strength of the nano composites during tests. 
Fig. 5 demonstrates the elongation of as cast copper-zinc amalgam and its composites. The rate prolongation was lessened 
in copper-zinc-ZrO2 composite when contrasted with the base combination. It very well may be seen from the diagram 
that the flexibility of the composites diminishes fundamentally with the 4, 8 and 12 wt. % nano ZrO2 fortified composites. 
This diminishing in rate prolongation in correlation with the base combinations is a most regularly happening burden in 
particulate fortified metal lattice composites. The lessened flexibility in copper-zinc-4, 8 and 12 wt. % composites can be 
ascribed to the nearness of ZrO2 particulates which may get broke and have sharp corners that make the composites 
inclined to confined break commencement and engendering. The embrittlement impact that happens because of the 
nearness of the hard-artistic particles causing expanded neighborhood stretch focus destinations may likewise be the 
reason [16]. 
 
 

 

Figure 4: Showing the ultimate tensile and yield strength of as 
cast copper alloy and copper-zinc-4, 8 and 12 wt. % nano ZrO2 
composite. 
 

 

Figure 5: Showing the percentage elongation of as cast copper 
alloy and copper-zinc-4, 8 and 12 wt. % nano ZrO2 composite. 
 

 
FRACTOGRAPHY 
 

he study of fractured surface of alloys & its composites becomes necessary to find the cause of failure of the 
fabricated materials. There are two important things to be remembered during analysis of fractography, a ductile 
material when fails there is a formation of small dimple like structure in the broken areas whereas in case of brittle 

fractures there is transgranular (fracture through grains) or inter-granular (fracture through grain boundaries) failures 
which can be observed in SEM images taken from a failed material. The fractured surfaces of copper-zinc along with 12 
wt. % of nano ZrO2 composite resulted from tension tests, are shown in fig. 6 (a-b). Fig. 6a represents the ductility 
fracture in copper-zinc alloy. SEM analysis of the fractured surfaces shows the dimpled fracture surface for the reinforced 
& unreinforced material. 

T 



 

                                                            P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35 
 

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                                                        (a)                                                                                      (b) 
 

Figure 6: SEM tensile fractured surfaces of (a) Copper-Zinc alloy (b) Copper-Zinc-12 wt.% of nano ZrO2 composites 
 
 
CONCLUSIONS 
 

n this research, by using stir casting fabrication technique the nano ZrO2/Copper-Zinc nano composites have been 
fabricated by considering 4, 8 and 12 wt. % of reinforcement. The micro-structural analysis, major mechanical 
behaviors like hardness, ultimate and yield strength, percentage elongation, and fractography behavior of prepared 

samples are studied as per ASTM standards. The matrix is almost free from pores in as cast alloy and uniformly 
distributed of nano particles in the prepared composite, which is evident from SEM microphotographs. The EDS analysis 
confirms the presence of nano ZrO2 particles in the Cu-Zn alloy matrix. Compared to unreinforced material the 
mechanical properties of Cu-Zn-4, 8 and 12 wt. % nano ZrO2 composite are superior and enhanced. Due to strain 
localization, the fracture surface of the composite material consists of small voids. 
 
 
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P.H. Nayak et alii, Frattura ed Integrità Strutturale, 48 (2019) 370-376; DOI: 10.3221/IGF-ESIS.48.35                                                                             
 

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    /HRV (Za stvaranje Adobe PDF dokumenata najpogodnijih za visokokvalitetni ispis prije tiskanja koristite ove postavke.  Stvoreni PDF dokumenti mogu se otvoriti Acrobat i Adobe Reader 5.0 i kasnijim verzijama.)
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    /NLD (Gebruik deze instellingen om Adobe PDF-documenten te maken die zijn geoptimaliseerd voor prepress-afdrukken van hoge kwaliteit. De gemaakte PDF-documenten kunnen worden geopend met Acrobat en Adobe Reader 5.0 en hoger.)
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    /UKR <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>
    /ENU (Use these settings to create Adobe PDF documents best suited for high-quality prepress printing.  Created PDF documents can be opened with Acrobat and Adobe Reader 5.0 and later.)
  >>
  /Namespace [
    (Adobe)
    (Common)
    (1.0)
  ]
  /OtherNamespaces [
    <<
      /AsReaderSpreads false
      /CropImagesToFrames true
      /ErrorControl /WarnAndContinue
      /FlattenerIgnoreSpreadOverrides false
      /IncludeGuidesGrids false
      /IncludeNonPrinting false
      /IncludeSlug false
      /Namespace [
        (Adobe)
        (InDesign)
        (4.0)
      ]
      /OmitPlacedBitmaps false
      /OmitPlacedEPS false
      /OmitPlacedPDF false
      /SimulateOverprint /Legacy
    >>
    <<
      /AddBleedMarks false
      /AddColorBars false
      /AddCropMarks false
      /AddPageInfo false
      /AddRegMarks false
      /ConvertColors /ConvertToCMYK
      /DestinationProfileName ()
      /DestinationProfileSelector /DocumentCMYK
      /Downsample16BitImages true
      /FlattenerPreset <<
        /PresetSelector /MediumResolution
      >>
      /FormElements false
      /GenerateStructure false
      /IncludeBookmarks false
      /IncludeHyperlinks false
      /IncludeInteractive false
      /IncludeLayers false
      /IncludeProfiles false
      /MultimediaHandling /UseObjectSettings
      /Namespace [
        (Adobe)
        (CreativeSuite)
        (2.0)
      ]
      /PDFXOutputIntentProfileSelector /DocumentCMYK
      /PreserveEditing true
      /UntaggedCMYKHandling /LeaveUntagged
      /UntaggedRGBHandling /UseDocumentProfile
      /UseDocumentBleed false
    >>
  ]
>> setdistillerparams
<<
  /HWResolution [2400 2400]
  /PageSize [612.000 792.000]
>> setpagedevice