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IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE)
e-ISSN: 2278-1684,p-ISSN: 2320-334X, Volume 12, Issue 1 Ver. III (Jan- Feb. 2015), PP 01-05
www.iosrjournals.org
DOI: 10.9790/1684-12130105 www.iosrjournals.org 1 | Page
Effect of Notch Angle on the Fracture Toughness of Al7075 T6
Alloy- An Experimental Approach
Trimbak K. Todkari1
, M. C. Swami2
, P. S. Patil3
1
(M.E. Machine Design Student of Mechanical Department, M. S. Bidve Engineering College,
Latur,Maharashtra,India.)
2
(Faculty of Mechanical Department, M. S. Bidve Engineering College, Latur, Maharashtra, India.)
3
(Faculty of Mechanical Department, G. N. D. Engineering College, Bidar, Karnataka, India.)
Abstract: In this paper fracture toughness (kIC) of Al7075 T6 alloy has been determined by using
circumferentially cracked round bar (CCRB) specimen having three notch angles (α) namely 450
,600
,750
respectively. The purpose of the study was to determine the effect notch angle on the fracture toughness of the
Al7075 T6 alloy. The obtained fracture toughness results for different notch are compared with ASTM
standards. The result shows that the notch angle has significant effect on the value of fracture toughness (KIC).
Keywords: Al7075 T6 alloy, CCRB specimen, Fracture toughness, notched specimen.
I. Introduction
The need of high strength, low weight, and more corrosion resistant material is of current interest in the
area of aerospace, marine etc. The Al 7075 T6 alloy material find wide applications in the different areas
because of its excellent metallurgical properties. The Al 7075 T6 alloy is made more useful material with the
characterization of material for fracture toughness. The determination of fracture toughness is based on the
stress intensity factor (KIC) at the crack tip with subscript I denotes the fracture toughness test is performed in
tensile mode and C denotes the critical value of stress intensity factor. When K attains critical value then crack
propagation becomes unstable and result in fracture of components [1].
Normally KIC is determined by using compact-tension (CT) specimen or single edge notch bend
(SENB) specimen or three point loaded bend specimens which are standardized by ASTM [14]. Also the
standard test method for fracture toughness (KIC) of metallic material is given by the American Society for
Testing and Material (ASTM) (designation E99) [2]. The ASTM E99 standard test method is to be one of the
most accurate ways of measuring KIC of low ductility high strength alloys [3].These methods are difficult and
also the preparation of specimen. Notched round bar specimens have widely used for finding mechanical
properties of materials [4-5]. The advantages of using circumferentially notched bars for fracture toughness
testing can be summarized as follows:
 The plane strain condition can be obtained because the circumferential crack has no end in the plane stress
region compared with the standard specimen geometries [6].
 Because of radial symmetry microstructure of the material along the circumferential area is completely
uniform [7].
 Preparation of CCRB specimen is easy.
 Fracture toughness test is easy to perform.
In the previous studies, Bayram et al. [8] measured fracture toughness KIC of various steels and
aluminum alloys with CCRB specimens and summarized that the experimentally measured fracture toughness
values using CCRB specimens are accurate and reliable considering some correction factors.
Christopher D. Wilson and John D. Landes [9] used circumferentially notched round bars with finite
notch root radii. They observed that the circumferential crack propagates radially inwards in tensile loading
unlike unique crack propagation towards one direction in case of CT or SENB specimens.
Wang Chang [10] determined the plane strain fracture toughness (KIC) by single cylindrical tensile
small scale specimen with ring-shaped crack.
NeelakanthaV Londe [11] determined the fracture toughness of metallic material by using CCRB
specimen having notch angle (450
) and unchanged outer diameter (D) with different notch diameter (d) of
Al6082-T6 alloy. They have found the value of KIC closer to standard tests.
Ali Bayram [8] determine the fracture toughness of metallic material using CCRB specimen having
notch angle (600
) and unchanged outer diameter (D) with different notch diameter (d) tested for different
metallic materials also find the fracture toughness by adding the correction factor. They have concluded that
fracture toughness measurement of metallic material using CCRB specimen is to be an accurate and reliable
procedure.
Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach
DOI: 10.9790/1684-12130105 www.iosrjournals.org 2 | Page
S K Nath [1] determine the fracture toughness of medium carbon steel using CCRB specimen having
different notch angles i.e. 450
,600
,750
and unchanged specimen diameter(D) with different notch diameter(d).
They have tested the material before heat treatment and after heat treatment and concluded that samples with
lower notch diameter shows higher KIC for same notch angle as compared to higher notch diameter.
The objective of the present work is to determine the effect of notch angle (α) on fracture toughness
and to validate the results with the standards. For the present study the ratio of D/d kept as constant and the ratio
is equal to 1.2 with varying notch angles. Also the effect of constant D/d ratio with different notch angles on
fracture toughness value by using CCRB specimen is investigated.
II. Theoretical Determination Of KIC
The determination of fracture toughness is based on the stress intensity factor (KIC) at the crack tip,
where I- denotes that the fracture toughness test is performed in tensile mode and C- denotes that the value of k
is critical. Unstable crack propagation occurs when K attains a critical value and the component fails. In Linear
Elastic Fracture Mechanics (LEFM) the critical Stress Intensity Factor (SIF) characterizes the fracture toughness
[12]. Wang. C.H et al. [13] have given an equation for calculating KIC of a CCRB specimen under tensile load
and is given in equation (1). This relation is valid for 1.2 ≤ D/d ≤ 2.1.
KIC= [0.932 Pf√D] / (d2
√π) (Eq1)
Where, Pf is the fracture load,
D is the diameter of the specimen, and d is the diameter of the notched section (Fig.1).
According to Dieter [14] for round notched tensile specimen, fracture toughness KIC found using following Eq.
KIC = Pf / (D)3/2
[1.72(D/d) -1.27] (Eq 2)
Where, Pf is the fracture load,
D is the diameter of the specimen, and d is the diameter of the notched section (Fig.1).
The assumption made while formulating above expression is that the specimen retains its elastic behavior until
fracture occurs. This relation is valid for the D/d ratio between 1.00 and 1.25.
III. Materials And Methods
The material used for present work is Al7075 T-6 alloy whose chemical composition are given in
Table. 1 and initially diameter of rod is 16mm.
Table: 1 Chemical composition of Al7075 T-6 alloy used, in wt%.
Al Cr Cu Fe Mg Mn Si Ti Zn
87.1-91.4 0.18-.28 1.2-2 Max 0.5 2.1-2.9 Max 0.3 Max 0.4 Max 0.2 5.1-6.1
The Mechanical properties 0f Al7075-T6 Alloy is given in Table. 2
Table: 2 Mechanical properties of Al7075 T-6 alloy
Property Values
Ultimate Tensile Strength 572 Mpa
Fracture Toughness (KIC in L-T direction) 29 Mpa√m
Fracture Toughness (KIC in T-L direction) 25 Mpa√m
3.1 Specimen preparation
The test specimen geometry is as shown in Fig. 1. Nine testing specimens have been prepared as per
standard specifications with following dimensions.
Specimen diameter (D): 10mm.
Gauge length (Lo): 5D.
Specimen length (L): 30D.
Notch diameter (d): 8.3mm.
Notch angle (α): 450
,600
,750
(Three notch angles have been used).
Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach
DOI: 10.9790/1684-12130105 www.iosrjournals.org 3 | Page
Fig. 1. Schematic representation of round notched tensile specimen
Fig. 2. Circumferentially crack round bar testing specimens
IV. Experimentation
The tensile test of each CCRB specimen was performed on 400KN Computerized Universal testing
machine at room temperature. The specimen was loaded under tension and the detailed results are shown in
table 3 and table 4.
V. Result And Discussions
The specimen having different notch angles loaded on UTM machine and results are recorded. Table 3
and 4 shows the experimental observations of maximum load and ultimate stress for each specimen respectively.
The plane-strain fracture toughness of Al 7075-T6 alloy tested using CCRB specimen geometry was found to be
in a range of 27.59 to 28.50 as per Eq. (1) and 29.00 to 29.95 as per Eq. (2) which is valid range of KIC for
Al7075-T6 alloy as available in literature obtained by standard tests. The average fracture toughness values
calculated using Eq. (1) and Eq. (2) are 28.06, 29.49 MPam1/2
respectively, it was observed that Eq. (1) results
lower values of fracture toughness than Eq. (2) and are shown in figure (3) having notch angle 450
,600
,750
respectively. The measurement of fracture toughness is based on the critical stress intensity factor (KIC) of the
test specimen under Mode-I loading condition. These two equations give KIC value in a valid range as available
in the literature using standard CT (Compact Tension) specimens. The variation of Fracture toughness versus
notch angle, was drawn for all the values of KIC determined using Eq.1 and Eq.2 as shown in Figure (3).The
tables 4 shows that the comparison between the ultimate tensile strength of unnotched specimen with the
notched specimen and it is observed that if notch angle increases the value of tensile strength of material also
increases.
Table 3: Details of Ultimate Stress, Fracture load, Fracture Toughness (KIC) values of Notch
Angle with variation in diameters.
Trial
No.
Notch
angle(α)
Specimen
diameter(D)
Notch
diameter(d)
Ultimate
Stress
(MPa)
Fracture
load (PF) in
KN
Fracture Toughness
KIC(MPa )
Eq 1 Eq 2
1 450
10 8.3 461 36.20 27.63 29.04
2 600
10 8.3 468 36.76 28.05 29.49
3 750
10 8.3 474 37.30 28.47 29.92
4 450
10 8.3 462 36.25 27.68 29.08
5 600
10 8.3 469 36.80 28.08 29.52
6 750
10 8.3 475 37.34 28.50 29.95
7 450
10 8.3 460 36.15 27.59 29.00
8 600
10 8.3 469 36.85 28.12 29.56
9 750
10 8.3 475 37.28 28.45 29.90
Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach
DOI: 10.9790/1684-12130105 www.iosrjournals.org 4 | Page
Table 4: Details of Ultimate stress of unnotched specimen and Notched specimen
5.1 Representation of KIC values as per Eq 1 and Eq2 on Graph with Different Notch Angles
Fig. 3. Variation in Fracture Toughness with Notch angle
VI. Conclusions
It observed that by seeing the graph the value of notch angle changes then the value of KIC also
changes. It has been observed that as notch angle increases the value of fracture toughness get increases and in
the literature survey it observed that decreasing notch angle decreases the fracture toughness value [1].
It has been observed that introducing notch to the test specimen the strength and % of elongation of the material
decreases, results brittle failure occurs.
Based on above discussion final conclusions are as follows:
1. Fracture toughness (KIC) of metallic material can be successfully determined by using round bar tensile
specimen and the obtained values are comparable with other method like compression tension (CT)
specimens.
2. The plane-strain fracture toughness of Al 7075-T6 alloy tested using CCRB specimen geometry was found
to be in a range of 27.59 to 28.50 as per Eq. (1) and 29.00 to 29.95 as per Eq. (2) as per Eq. (2) which is
valid range of KIC for Al7075-T6 as available in literature obtained by standard tests
3. Introducing of notch in a tensile test specimen the % of elongation gets decreases.
4. Introduction of notch in tensile test specimen causes brittle failure although material will be ductile.
5. As a notch angle increases the value of KIC also increases.
Acknowledgements
I would like to thank Prof.M.C.Swami for Motivating me to undertake the project in Effect of Notch
Angle on theFracture Toughness of Al7075 T6 Alloy- An Experimental Approach I would like to thankful
Prof.S.G.Mantri and Prof.K.S.Upase providing me the Technical Knowledge about this project.
References
[1]. S.K. Nath and Uttam Kr Das: Effect of microstructure and notches on the fracture toughness of medium carbon steel, Journal of
Novel Architecture and Marine Engineering June,2006.
[2]. Anon: ASTM Designation E399, Standard Test Method for Plane-Strain Fracture Toughness of Metallic Materials in Annual Book
ofASTM Standards, Part 3, American Society for Testing and Materials,Philadelphia, PA, 1988, pp. 680-715.
[3]. S. Kang and N.J. Grant: Notch Tensile Testing as a Measure of the Toughness of Aluminum Alloys, Mat. Sci. Eng., 1985, 72, pp.
155-62.
[4]. K. Kobayashi, H. Imada, and T. Majima: Nucleation and Growth ofCreep Voids in Circumferentially Notched Specimens,” JSME
Int.J.A.-Solid M., 1998, 41, pp. 218-24.
Trial
No.
Notch
angle(α)
Specimen
diameter(D)
Notch
diameter(d)
Ultimate
Stress
(MPa)
1 00
10 - 530
2 450
10 8.3 461
3 600
10 8.3 468
4 750
10 8.3 474
5 45 10 8.3 462
6 60 10 8.3 469
7 75 10 8.3 475
8 45 10 8.3 460
9 60 10 8.3 469
10 75 10 8.3 475
Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach
DOI: 10.9790/1684-12130105 www.iosrjournals.org 5 | Page
[5]. A. Valiente and J. Lapena: Measurement of the Yield and TensileStrengths of Neutron-Irradiated and Post-Irradiation Recovered
VesselSteels with Notched Specimens,Nucl. Eng. Des, 1996, 167(1), pp.11-22.
[6]. D.M. Li and A. Bakker: Fracture Toughness Evaluation for an RSPAl Alloy Using Circumferentially-Cracked Cylindrical Bar
Specimens,Eng. Fract. Mech., 1997, 57, pp. 1-11.
[7]. B. Ule, B. Leskocsek, and B. Tuma: Estimation of Plane Strain FractureToughness of AISI M2 Steel FromPrecracked Round-Bar
Specimens,Eng. Fract. Mech., 2000, 65, pp. 559-72.
[8]. Ali Bayram; AgahUguz; Ali Durmus.(2002):Rapid determination of the fracture toughness of metallic materials using
circumferentiallynotched bars. J. Mater. Eng. Perform. 11(5), pp, 571-576.
[9]. Christopher D. Wilson; John D. Landes. (2000): Fracture toughness testing with notched round bars. Fatigue and Fracture
Mechanics 30,ASTM STP 1360, pp.69-82.
[10]. Wang Chang. (1987): Measurement of fracture toughness KIC by single small-scale cylindrical specimen with ring-shaped crack.
EFM,28(3), pp.241-250.
[11]. Neelakantha V Londe: Use of round bar specimen in fracture toughness test of metallic materials, International Journal Of
Engineering Science and Technology Vol.2(9),2010,4130-4136.
[12]. Marc Scibetta; RachidChaouadi; E.VanWalle. (2000): Fracture toughness analysis of circumferentially cracked bars. Int. J
Fract.,104,pp.145-168
[13]. Wang.C.H.(1996):Introduction to Fracture Mechanics; Stress analysis of cracked bodies. Aeronautical and Maritime Research
Laboratory.Victoria 3001, Melbourne, DSTO-GD-0103, pp.10-28.
[14]. Dieter, G. E. (1988): Mechanical Metallurgy, SI ed., McGraw-Hill, Singapore, pp.348-368.

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Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach

  • 1. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE) e-ISSN: 2278-1684,p-ISSN: 2320-334X, Volume 12, Issue 1 Ver. III (Jan- Feb. 2015), PP 01-05 www.iosrjournals.org DOI: 10.9790/1684-12130105 www.iosrjournals.org 1 | Page Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach Trimbak K. Todkari1 , M. C. Swami2 , P. S. Patil3 1 (M.E. Machine Design Student of Mechanical Department, M. S. Bidve Engineering College, Latur,Maharashtra,India.) 2 (Faculty of Mechanical Department, M. S. Bidve Engineering College, Latur, Maharashtra, India.) 3 (Faculty of Mechanical Department, G. N. D. Engineering College, Bidar, Karnataka, India.) Abstract: In this paper fracture toughness (kIC) of Al7075 T6 alloy has been determined by using circumferentially cracked round bar (CCRB) specimen having three notch angles (α) namely 450 ,600 ,750 respectively. The purpose of the study was to determine the effect notch angle on the fracture toughness of the Al7075 T6 alloy. The obtained fracture toughness results for different notch are compared with ASTM standards. The result shows that the notch angle has significant effect on the value of fracture toughness (KIC). Keywords: Al7075 T6 alloy, CCRB specimen, Fracture toughness, notched specimen. I. Introduction The need of high strength, low weight, and more corrosion resistant material is of current interest in the area of aerospace, marine etc. The Al 7075 T6 alloy material find wide applications in the different areas because of its excellent metallurgical properties. The Al 7075 T6 alloy is made more useful material with the characterization of material for fracture toughness. The determination of fracture toughness is based on the stress intensity factor (KIC) at the crack tip with subscript I denotes the fracture toughness test is performed in tensile mode and C denotes the critical value of stress intensity factor. When K attains critical value then crack propagation becomes unstable and result in fracture of components [1]. Normally KIC is determined by using compact-tension (CT) specimen or single edge notch bend (SENB) specimen or three point loaded bend specimens which are standardized by ASTM [14]. Also the standard test method for fracture toughness (KIC) of metallic material is given by the American Society for Testing and Material (ASTM) (designation E99) [2]. The ASTM E99 standard test method is to be one of the most accurate ways of measuring KIC of low ductility high strength alloys [3].These methods are difficult and also the preparation of specimen. Notched round bar specimens have widely used for finding mechanical properties of materials [4-5]. The advantages of using circumferentially notched bars for fracture toughness testing can be summarized as follows:  The plane strain condition can be obtained because the circumferential crack has no end in the plane stress region compared with the standard specimen geometries [6].  Because of radial symmetry microstructure of the material along the circumferential area is completely uniform [7].  Preparation of CCRB specimen is easy.  Fracture toughness test is easy to perform. In the previous studies, Bayram et al. [8] measured fracture toughness KIC of various steels and aluminum alloys with CCRB specimens and summarized that the experimentally measured fracture toughness values using CCRB specimens are accurate and reliable considering some correction factors. Christopher D. Wilson and John D. Landes [9] used circumferentially notched round bars with finite notch root radii. They observed that the circumferential crack propagates radially inwards in tensile loading unlike unique crack propagation towards one direction in case of CT or SENB specimens. Wang Chang [10] determined the plane strain fracture toughness (KIC) by single cylindrical tensile small scale specimen with ring-shaped crack. NeelakanthaV Londe [11] determined the fracture toughness of metallic material by using CCRB specimen having notch angle (450 ) and unchanged outer diameter (D) with different notch diameter (d) of Al6082-T6 alloy. They have found the value of KIC closer to standard tests. Ali Bayram [8] determine the fracture toughness of metallic material using CCRB specimen having notch angle (600 ) and unchanged outer diameter (D) with different notch diameter (d) tested for different metallic materials also find the fracture toughness by adding the correction factor. They have concluded that fracture toughness measurement of metallic material using CCRB specimen is to be an accurate and reliable procedure.
  • 2. Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach DOI: 10.9790/1684-12130105 www.iosrjournals.org 2 | Page S K Nath [1] determine the fracture toughness of medium carbon steel using CCRB specimen having different notch angles i.e. 450 ,600 ,750 and unchanged specimen diameter(D) with different notch diameter(d). They have tested the material before heat treatment and after heat treatment and concluded that samples with lower notch diameter shows higher KIC for same notch angle as compared to higher notch diameter. The objective of the present work is to determine the effect of notch angle (α) on fracture toughness and to validate the results with the standards. For the present study the ratio of D/d kept as constant and the ratio is equal to 1.2 with varying notch angles. Also the effect of constant D/d ratio with different notch angles on fracture toughness value by using CCRB specimen is investigated. II. Theoretical Determination Of KIC The determination of fracture toughness is based on the stress intensity factor (KIC) at the crack tip, where I- denotes that the fracture toughness test is performed in tensile mode and C- denotes that the value of k is critical. Unstable crack propagation occurs when K attains a critical value and the component fails. In Linear Elastic Fracture Mechanics (LEFM) the critical Stress Intensity Factor (SIF) characterizes the fracture toughness [12]. Wang. C.H et al. [13] have given an equation for calculating KIC of a CCRB specimen under tensile load and is given in equation (1). This relation is valid for 1.2 ≤ D/d ≤ 2.1. KIC= [0.932 Pf√D] / (d2 √π) (Eq1) Where, Pf is the fracture load, D is the diameter of the specimen, and d is the diameter of the notched section (Fig.1). According to Dieter [14] for round notched tensile specimen, fracture toughness KIC found using following Eq. KIC = Pf / (D)3/2 [1.72(D/d) -1.27] (Eq 2) Where, Pf is the fracture load, D is the diameter of the specimen, and d is the diameter of the notched section (Fig.1). The assumption made while formulating above expression is that the specimen retains its elastic behavior until fracture occurs. This relation is valid for the D/d ratio between 1.00 and 1.25. III. Materials And Methods The material used for present work is Al7075 T-6 alloy whose chemical composition are given in Table. 1 and initially diameter of rod is 16mm. Table: 1 Chemical composition of Al7075 T-6 alloy used, in wt%. Al Cr Cu Fe Mg Mn Si Ti Zn 87.1-91.4 0.18-.28 1.2-2 Max 0.5 2.1-2.9 Max 0.3 Max 0.4 Max 0.2 5.1-6.1 The Mechanical properties 0f Al7075-T6 Alloy is given in Table. 2 Table: 2 Mechanical properties of Al7075 T-6 alloy Property Values Ultimate Tensile Strength 572 Mpa Fracture Toughness (KIC in L-T direction) 29 Mpa√m Fracture Toughness (KIC in T-L direction) 25 Mpa√m 3.1 Specimen preparation The test specimen geometry is as shown in Fig. 1. Nine testing specimens have been prepared as per standard specifications with following dimensions. Specimen diameter (D): 10mm. Gauge length (Lo): 5D. Specimen length (L): 30D. Notch diameter (d): 8.3mm. Notch angle (α): 450 ,600 ,750 (Three notch angles have been used).
  • 3. Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach DOI: 10.9790/1684-12130105 www.iosrjournals.org 3 | Page Fig. 1. Schematic representation of round notched tensile specimen Fig. 2. Circumferentially crack round bar testing specimens IV. Experimentation The tensile test of each CCRB specimen was performed on 400KN Computerized Universal testing machine at room temperature. The specimen was loaded under tension and the detailed results are shown in table 3 and table 4. V. Result And Discussions The specimen having different notch angles loaded on UTM machine and results are recorded. Table 3 and 4 shows the experimental observations of maximum load and ultimate stress for each specimen respectively. The plane-strain fracture toughness of Al 7075-T6 alloy tested using CCRB specimen geometry was found to be in a range of 27.59 to 28.50 as per Eq. (1) and 29.00 to 29.95 as per Eq. (2) which is valid range of KIC for Al7075-T6 alloy as available in literature obtained by standard tests. The average fracture toughness values calculated using Eq. (1) and Eq. (2) are 28.06, 29.49 MPam1/2 respectively, it was observed that Eq. (1) results lower values of fracture toughness than Eq. (2) and are shown in figure (3) having notch angle 450 ,600 ,750 respectively. The measurement of fracture toughness is based on the critical stress intensity factor (KIC) of the test specimen under Mode-I loading condition. These two equations give KIC value in a valid range as available in the literature using standard CT (Compact Tension) specimens. The variation of Fracture toughness versus notch angle, was drawn for all the values of KIC determined using Eq.1 and Eq.2 as shown in Figure (3).The tables 4 shows that the comparison between the ultimate tensile strength of unnotched specimen with the notched specimen and it is observed that if notch angle increases the value of tensile strength of material also increases. Table 3: Details of Ultimate Stress, Fracture load, Fracture Toughness (KIC) values of Notch Angle with variation in diameters. Trial No. Notch angle(α) Specimen diameter(D) Notch diameter(d) Ultimate Stress (MPa) Fracture load (PF) in KN Fracture Toughness KIC(MPa ) Eq 1 Eq 2 1 450 10 8.3 461 36.20 27.63 29.04 2 600 10 8.3 468 36.76 28.05 29.49 3 750 10 8.3 474 37.30 28.47 29.92 4 450 10 8.3 462 36.25 27.68 29.08 5 600 10 8.3 469 36.80 28.08 29.52 6 750 10 8.3 475 37.34 28.50 29.95 7 450 10 8.3 460 36.15 27.59 29.00 8 600 10 8.3 469 36.85 28.12 29.56 9 750 10 8.3 475 37.28 28.45 29.90
  • 4. Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach DOI: 10.9790/1684-12130105 www.iosrjournals.org 4 | Page Table 4: Details of Ultimate stress of unnotched specimen and Notched specimen 5.1 Representation of KIC values as per Eq 1 and Eq2 on Graph with Different Notch Angles Fig. 3. Variation in Fracture Toughness with Notch angle VI. Conclusions It observed that by seeing the graph the value of notch angle changes then the value of KIC also changes. It has been observed that as notch angle increases the value of fracture toughness get increases and in the literature survey it observed that decreasing notch angle decreases the fracture toughness value [1]. It has been observed that introducing notch to the test specimen the strength and % of elongation of the material decreases, results brittle failure occurs. Based on above discussion final conclusions are as follows: 1. Fracture toughness (KIC) of metallic material can be successfully determined by using round bar tensile specimen and the obtained values are comparable with other method like compression tension (CT) specimens. 2. The plane-strain fracture toughness of Al 7075-T6 alloy tested using CCRB specimen geometry was found to be in a range of 27.59 to 28.50 as per Eq. (1) and 29.00 to 29.95 as per Eq. (2) as per Eq. (2) which is valid range of KIC for Al7075-T6 as available in literature obtained by standard tests 3. Introducing of notch in a tensile test specimen the % of elongation gets decreases. 4. Introduction of notch in tensile test specimen causes brittle failure although material will be ductile. 5. As a notch angle increases the value of KIC also increases. Acknowledgements I would like to thank Prof.M.C.Swami for Motivating me to undertake the project in Effect of Notch Angle on theFracture Toughness of Al7075 T6 Alloy- An Experimental Approach I would like to thankful Prof.S.G.Mantri and Prof.K.S.Upase providing me the Technical Knowledge about this project. References [1]. S.K. Nath and Uttam Kr Das: Effect of microstructure and notches on the fracture toughness of medium carbon steel, Journal of Novel Architecture and Marine Engineering June,2006. [2]. Anon: ASTM Designation E399, Standard Test Method for Plane-Strain Fracture Toughness of Metallic Materials in Annual Book ofASTM Standards, Part 3, American Society for Testing and Materials,Philadelphia, PA, 1988, pp. 680-715. [3]. S. Kang and N.J. Grant: Notch Tensile Testing as a Measure of the Toughness of Aluminum Alloys, Mat. Sci. Eng., 1985, 72, pp. 155-62. [4]. K. Kobayashi, H. Imada, and T. Majima: Nucleation and Growth ofCreep Voids in Circumferentially Notched Specimens,” JSME Int.J.A.-Solid M., 1998, 41, pp. 218-24. Trial No. Notch angle(α) Specimen diameter(D) Notch diameter(d) Ultimate Stress (MPa) 1 00 10 - 530 2 450 10 8.3 461 3 600 10 8.3 468 4 750 10 8.3 474 5 45 10 8.3 462 6 60 10 8.3 469 7 75 10 8.3 475 8 45 10 8.3 460 9 60 10 8.3 469 10 75 10 8.3 475
  • 5. Effect of Notch Angle on the Fracture Toughness of Al7075 T6 Alloy- An Experimental Approach DOI: 10.9790/1684-12130105 www.iosrjournals.org 5 | Page [5]. A. Valiente and J. Lapena: Measurement of the Yield and TensileStrengths of Neutron-Irradiated and Post-Irradiation Recovered VesselSteels with Notched Specimens,Nucl. Eng. Des, 1996, 167(1), pp.11-22. [6]. D.M. Li and A. Bakker: Fracture Toughness Evaluation for an RSPAl Alloy Using Circumferentially-Cracked Cylindrical Bar Specimens,Eng. Fract. Mech., 1997, 57, pp. 1-11. [7]. B. Ule, B. Leskocsek, and B. Tuma: Estimation of Plane Strain FractureToughness of AISI M2 Steel FromPrecracked Round-Bar Specimens,Eng. Fract. Mech., 2000, 65, pp. 559-72. [8]. Ali Bayram; AgahUguz; Ali Durmus.(2002):Rapid determination of the fracture toughness of metallic materials using circumferentiallynotched bars. J. Mater. Eng. Perform. 11(5), pp, 571-576. [9]. Christopher D. Wilson; John D. Landes. (2000): Fracture toughness testing with notched round bars. Fatigue and Fracture Mechanics 30,ASTM STP 1360, pp.69-82. [10]. Wang Chang. (1987): Measurement of fracture toughness KIC by single small-scale cylindrical specimen with ring-shaped crack. EFM,28(3), pp.241-250. [11]. Neelakantha V Londe: Use of round bar specimen in fracture toughness test of metallic materials, International Journal Of Engineering Science and Technology Vol.2(9),2010,4130-4136. [12]. Marc Scibetta; RachidChaouadi; E.VanWalle. (2000): Fracture toughness analysis of circumferentially cracked bars. Int. J Fract.,104,pp.145-168 [13]. Wang.C.H.(1996):Introduction to Fracture Mechanics; Stress analysis of cracked bodies. Aeronautical and Maritime Research Laboratory.Victoria 3001, Melbourne, DSTO-GD-0103, pp.10-28. [14]. Dieter, G. E. (1988): Mechanical Metallurgy, SI ed., McGraw-Hill, Singapore, pp.348-368.