ISO 26843:2015

INTERNATIONAL ISO
STANDARD 26843
First edition
2015-12-15
Metallic materials — Measurement
of fracture toughness at impact
loading rates using precracked
Charpy-type test pieces
Matériaux métalliques — Mesure de la ténacité d’éprouvettes type
Charpy préfissurées soumises à un chargement d’impact
Reference number
ISO 26843:2015(E)
©
ISO 2015

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ISO 26843:2015(E)

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© ISO 2015, Published in Switzerland
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ISO 26843:2015(E)

Contents Page
Foreword .iv
Introduction .v
1 Scope . 1
2 Normative references . 1
3 Symbols . 1
4 Principle . 3
5 Test specimens. 5
6 Testing machines . 6
7 Test procedures and measurements. 6
7.1 General . 6
7.2 Impact velocity . 7
7.3 Time to fracture . 7
7.4 Multiple specimen tests. 7
7.5 Single-specimen tests . 7
7.6 Post-test crack length measurements . 8
8 Evaluation of fracture mechanics parameters . 8
9 Test report . 9
9.1 Organization . 9
9.2 Specimen, material, and test environment . 9
9.2.1 Specimen description . 9
9.2.2 Specimen dimensions . 9
9.2.3 Material description . . 9
9.2.4 Test environment .10
9.3 Fatigue precracking conditions .10
9.4 Test data qualification .10
9.4.1 Limitations .10
9.4.2 Crack length measurements .10
9.4.3 Fracture surface appearance .10
9.4.4 Resistance curves .10
9.4.5 Checklist for data qualification .10
9.5 Test results.11
Annex A (normative) Test machines suitable for each test procedure .12
Annex B (informative) Estimation of strain rate .13
Annex C (normative) Dynamic evaluation of fracture toughness .14
Annex D (normative) Determination of resistance curves at impact loading rates by
multiple specimen methods .19
Annex E (normative) Estimation of J-Δa R-curves using the normalization method .21
d
Annex F (normative) Determination of characteristic fracture toughness value J .24
0,2Bd
Annex G (normative) Validity criteria .25
Annex H (normative) Determination of fracture toughness in terms of J-integral .27
Annex I (informative) Example test reports .29
Bibliography .34
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ISO 26843:2015(E)

Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards
bodies (ISO member bodies). The work of preparing International Standards is normally carried out
through ISO technical committees. Each member body interested in a subject for which a technical
committee has been established has the right to be represented on that committee. International
organizations, governmental and non-governmental, in liaison with ISO, also take part in the work.
ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of
electrotechnical standardization.
The procedures used to develop this document and those intended for its further maintenance are
described in the ISO/IEC Directives, Part 1. In particular the different approval criteria needed for the
different types of ISO documents should be noted. This document was drafted in accordance with the
editorial rules of the ISO/IEC Directives, Part 2 (see www.iso.org/directives).
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of
any patent rights identified during the development of the document will be in the Introduction and/or
on the ISO list of patent declarations received (see www.iso.org/patents).
Any trade name used in this document is information given for the convenience of users and does not
constitute an endorsement.
For an explanation on the meaning of ISO specific terms and expressions related to conformity
assessment, as well as information about ISO’s adherence to the WTO principles in the Technical
Barriers to Trade (TBT) see the following URL: Foreword - Supplementary information
The committee responsible for this document is ISO/TC 164, Mechanical testing of metals, Subcommittee
SC 4, Toughness testing — Fracture (F), Pendulum (P), Tear (T).
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ISO 26843:2015(E)

Introduction
This International Standard is closely related to ISO 14556 and was derived from a draft procedure
prepared by the Working Party “European Standards on Instrumented Precracked Charpy Testing”
of the European Structural Integrity Society (ESIS) Technical Subcommittee on Dynamic Testing at
Intermediate Strain Rates (TC5).
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INTERNATIONAL STANDARD ISO 26843:2015(E)
Metallic materials — Measurement of fracture toughness
at impact loading rates using precracked Charpy-type test
pieces
1 Scope
This International Standard specifies requirements for performing and evaluating instrumented
precracked Charpy impact tests on metallic materials using a fracture mechanics approach. Minimum
requirements are given for measurement and recording equipment such that similar sensitivity and
comparable measurements are achieved.
Dynamic fracture mechanics properties determined using this International Standard are comparable
with conventional large-scale fracture mechanics results when the corresponding validity criteria are
met. Because of the small absolute size of the Charpy specimen, this is often not the case. Nevertheless,
the values obtained can be used in research and development of materials, in quality control, and to
establish the variation of properties with test temperature under impact loading rates.
Fracture toughness properties determined through the use of this International Standard may differ
from values measured at quasistatic loading rates. Indeed, an increase in loading rate causes a decrease
in fracture toughness when tests are performed in the brittle or ductile-to-brittle regimes; the opposite
is observed (i.e. increase in fracture toughness) in the fully ductile regime. More information on the
dependence of fracture toughness on loading (or strain) rate is given in Reference [1]. In addition, it is
generally acknowledged that fracture toughness also depends on test temperature. For these reasons,
the user is required to report the actual test temperature and loading rate for each test performed.
In case of cleavage fracture of ferritic steels in the ductile-to-brittle transition region, variability can
be very large and cannot be adequately described by simple statistics. In this case, additional tests are
required and the analysis is to be performed using a statistical procedure applicable to this type of test,
see for example Reference [2].
NOTE Modifications to the analytical procedures prescribed in Reference [2] might be necessary to account
for the effect of elevated (impact) loading rates.
2 Normative references
The following documents, in whole or in part, are normatively referenced in this document and are
indispensable for its application. For dated references, only the edition cited applies. For undated
references, the latest edition of the referenced document (including any amendments) applies.
ISO 148-1, Metallic materials — Charpy pendulum impact test — Part 1: Test method
ISO 148-2, Metallic materials — Charpy pendulum impact test — Part 2: Verification of testing machines
ISO 12135, Metallic materials — Unified method of test for the determination of quasistatic fracture toughness
ISO 14556, Steel — Charpy V-notch pendulum impact test — Instrumented test method
ISO 26203-2, Metallic materials — Tensile testing at high strain rates — Part 2: Servo-hydraulic and
other test systems
3 Symbols
For the purposes of this International Standard, the following symbols given in Table 1 apply.
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ISO 26843:2015(E)

Table 1 — Symbols and definitions used in this International Standard
Symbol Definition Unit
Nominal crack length (for the purposes of fatigue precracking, an assigned value less mm
a
than a )
0
a Final crack length (a + Δa) mm
f 0
a Length of machined notch mm
m
a Initial crack length mm
0
Δa Crack extension (a – a ) mm
0
Δa Crack extension limit for J-controlled crack extension mm
max
Δa Crack extension corresponding to displacement s mm
s
B Specimen thickness mm
B Specimen effective thickness as defined in Formula (E.7) mm
e
B Specimen net thickness after side-grooving mm
N
C Compliance of the test machine m/N
M
C Specimen elastic compliance m/N
0
C Specimen theoretical compliance m/N
S
E Young’s modulus of elasticity GPa
−1
dε/dt Strain rate s
f Output frequency limit Hz
g
F Applied force N
F Applied force at onset of unstable crack extension in Figure 1 N
cd
F Maximum fatigue precracking force during the final precracking stage N
f
F Applied force at onset of general yielding as defined in ISO 14556 N
gy
F Maximum applied force as defined in ISO 14556 N
m
F Applied force corresponding to a displacement s N
s
2
J Dynamic J-integral MJ/m
d
2
J Dynamic equivalent of J in ISO 12135 (with B = 10 mm) MJ/m
cd c(B)
2
J J at upper limit of J-controlled crack extension MJ/m
g
2
J Limit of J -R material behaviour defined by this test method MJ/m
d,max d
2
J Dynamic equivalent of J in ISO 12135 (with B = 10 mm) MJ/m
ud u(B)
2
J Dynamic equivalent of J in ISO 12135 (with B = 10 mm) MJ/m
0,2Bd 0,2BL(B)
2 −1
dJ /dt Rate of change of dynamic J-integral MJ/m s
d
0,5
K Dynamic stress intensity factor MPa m
d
0,5
K Dynamic stress intensity factor calculated from J-integral MPa m
Jd
dyn 0,5
K (t) Stress intensity factor – time history from the impact response curve method MPa m
I
0,5
K Dynamic plane strain fracture toughness MPa m
Id
0,5
K Dynamic stress intensity factor calculated from J-integral at the onset of cleavage MPa m
Jcd
0,5 −1
dK /dt Rate of change of dynamic stress intensity factor MPa m s
d
KV Absorbed energy as defined in ISO 148-1 J
KV Available potential energy corresponding to a reduced pendulum impact velocity v J
0 0
M Total mass of the moving striker of the pendulum kg
n Strain hardening exponent of the Ramberg-Osgood material law —
N Number of available test specimens —
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ISO 26843:2015(E)

Table 1 (continued)
Symbol Definition Unit
Dynamic flow stress, defined as the average of dynamic yield strength and dynamic
R MPa
fd
tensile strength
R Dynamic tensile strength determined at the strain rate of the fracture toughness test MPa
md
Dynamic yield (proof) strength determined at the strain rate of the fracture tough-
R MPa
pd
ness test
R Yield (proof) strength measured at quasistatic strain rate MPa
p
s Specimen displacement (calculated according to ISO 14556) mm
s Plastic component of specimen displacement mm
pl
S Span between outer loading points mm
T Temperature °C
t Time s
t Time to fracture s
f
t Time at the onset of crack propagation s
i
t Signal rise time s
r
t Time at striker impact s
o
τ Period of force oscillation s
−1
v Initial striker impact velocity m s
0
v Striker impact velocity corresponding to the maximum available energy of the pendu-
0s
−1
m s
lum
W Specimen effective width mm
W Energy at maximum force as defined in ISO 14556 J
m
W Plastic component of the area under the force-displacement test record up to displace-
p
J
ment s
W Total fracture energy under the force-displacement test record up to displacement s J
s
W Calculated energy from area under complete force-displacement test record up to
t
J
F = 0,02 F as defined in ISO 14556
m
W Available impact energy J
o
ν Poisson’s ratio —
4 Principle
This International Standard prescribes impact bend tests which may be performed on fatigue precracked
Charpy-type specimens to obtain dynamic fracture mechanics properties of metallic materials. This
International Standard extends the procedure for V-notch impact bend tests in accordance with
ISO 148-1, and may be used for the evaluation of the master curve reference temperature in accordance
with Reference [2] provided that the corresponding validity requirements are met. Instrumented
testing machines are required together with ancillary instrumentation and recording equipment in
accordance with ISO 14556.
Fracture toughness properties depend on material response reflected in the force-time diagrams
described in Table 2 and Figure 1. The logical structure for fracture property determination and
validation is shown in the flow chart of Figure 2.
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ISO 26843:2015(E)

Table 2 — Fracture toughness properties to be determined
Material response/fracture behaviour Corresponding diagram type R-curve Characteristic pa-
(see Figure 1) rameters
J , K , K (B, dK /
cd Jcd Id d
Linear-elastic I —
dt, dJ /dt)
d
Elastic-plastic, unstable fracture with
II — J , K (B,dJ /dt)
cd Jcd d
Δa < 0,2 mm
Elastic-plastic, unstable fracture with
II — J (B,Δa,dJ /dt)
ud d
0,2 mm ≤ Δa ≤ 0,15 (W − a )
0
Elastic-plastic, unstable fracture with
III J -Δa J (dJ /dt)
d 0,2Bd d
Δa > 0,15 (W − a )
0
Elastic-plastic; no unstable fracture IV J -Δa J (dJ /dt)
d 0,2Bd d
Force
Force
Type I
F
Type II
cd
F
cd
t t
Force Time Time
f f
Force
Type III
F
m F
m
Type IV
F
cd
Test
F
gy
termination
F
gy
Figure 1 — Typical force-time diagrams (schematic)
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ISO 26843:2015(E)

Fracture toughness test
at impact loading rates
Unstable Fracture
Stable
Figure 1 types I or II behaviour
Figure 1 types III or IV
Figure 1
II
I
type
Test method
No Yes
Yes No
t < 3τ
t < 3τ
f
f
Use lower
Quasistatic Quasistatic
Use lower Multi-specimen
Single-specimen
impact
impact elastic-plastic
elastic-plastic
evaluation
normalization
velocity
velocity
fracture fracture
method
method
or
mechanics mechanics
dynamic eval.
(Annex E)
(Annex H) (Annex H)
(Annex D)
methods
(Annex C)
repeat test with
different ∆a
J , K J , K , J
K
Id cd Jcd cd Jcd ud
J-R curve
No
No
Yes
0,2 ≤ ∆a ≤ 0,15
∆a < 0,2 mm
AnneAnnex Fx F
(W−a )
0
Yes
J , K J
JJ , , KK
Validity (Annex G) Validity (Annex G)
cd Jcd ud
cdcd JcJcdd
Figure 2 — Flow chart for the application of the test method
5 Test specimens
5.1 Specimens shall be prepared in accordance with the standard specimens of ISO 148-1, with or
without the 2,0 mm V-notch, followed by fatigue precracking.
5.2 Specimens shall be fatigue precracked in bending to produce an initial crack length, a , in the range
0
0,30 ≤ a /W ≤ 0,70.
0
If the results in terms of J are to be directly comparable with full-size standard fracture toughness
values such as J (as defined in ISO 12135), then a /W shall be in the range 0,45 < a /W < 0,70.
0,2BL 0 0
Shorter crack lengths may be more advantageous, as a stiffer test piece increases the probability of a
successful test.
5.3 To initiate fatigue precracking, machine or spark erode a slot into the specimen. For specimens
with an existing V-notch, fatigue precracking may initiate at the bottom of the notch. The length of the
machined notch, a , shall be at least 1,0 mm shorter than the desired initial crack length, a .
m 0
5.4 During the final 1,3 mm or 50 % of precrack extension, whichever is less, the maximum fatigue
precracking force shall be the lower of:
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ISO 26843:2015(E)

2
0,8BW−a
()
0
F= R (1)
f p
S
or
 
 
WBB
W 
N
 
F=ξ×E (2)
f  
 a   S
 
0
f
   
W
 
 
a
 
0
−4 1/2
where ξ = 1,6 × 10 m and the function f is given in Formula (H.2).
 
W
 
The ratio of minimum-to-maximum fatigue precracking force shall be in the range 0 to 0,1 except that
to expedite crack initiation one or more cycles of −1,0 may be first applied.
NOTE For plain-sided specimens, B = B.
N
5.5 When fatigue precracking is performed at temperature T and testing is performed at temperature
1
T , F in Formula (2) shall be factored by the ratio R [T ] / R [T ], where R [T ] is the quasistatic yield
2 f p 1 pd 2 p 1
strength at temperature T and R [T ] is the dynamic yield strength at temperature T . In addition, F
1 pd 2 2 f
determined from Formula (1) shall be evaluated using the smaller value of R [T ] and R [T ].
p 1 pd 2
5.6 Specimens may be side grooved, preferably after fatigue precracking, using a V-notch cutter in
accordance with ISO 148-1 to a depth of 1,0 mm on each side. Side grooving is recommended for all J -Δa
d
R-curve tests. For details of crack length measurement, see 9.4.2.
6 Testing machines
6.1 The tests may be carried out using testing machines of the general types specified in Annex A. Not
all machines can perform all types of test (see Annex A for more details). In all cases, the striker and anvil
dimensions shall conform to ISO 148-2.
6.2 Details of machine instrumentation and calibration procedures are specified in ISO 14556.
6.3 For every test in which the entire force signal has been recorded (i.e. the force returns to the
baseline), the difference between KV and W shall be within ±15 % of KV or ±1 J, whichever is larger. If
t
this requirement is not met but the difference does not exceed ±25 % of KV or ±2 J, whichever is larger,
[3]
force values may be adjusted until KV = W . If the difference exceeds ±25 % of KV or ±2 J, whichever is
t
larger, the test shall be discarded and the calibration of the instrumented striker user shall be checked
and if necessary repeated. If recording of the entire force signal is not possible (for example due to the
specimen being ejected from the machine without being fully broken), conformance to the requirements
stated earlier shall be demonstrated by testing, using the same experimental apparatus, at least five
Charpy specimens (precracked, non-precracked, or a mix of precracked and non-precracked) of similar
absorbed energy level, for which the entire force signal is recorded. In all cases, the difference between
KV and W shall be within ±15 % of KV or ±1 J, whichever is larger.
t
7 Test procedures and measurements
7.1 General
Tests are performed in general accordance with the standard Charpy impact test of ISO 148-1, with
allowance for other types of machines, as specified in Annex A.
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ISO 26843:2015(E)

The force-displacement diagram is recorded according to ISO 14556, from which the key data values
F , F , W , and W are determined. In addition to the procedures of ISO 14556, specific procedures for
m cd m t
determining striking velocity, available energy, and crack lengths are given below. These data form the
basis for evaluation of toughness parameters according to Annexes D to F.
NOTE The force F in this International Standard corresponds to the force F (crack initiation force) in
cd iu
ISO 14556.
7.2 Impact velocity
This International Standard applies to any impact velocity, v , in excess of those corresponding to
0
the testing rates prescribed by ISO 12135. Commonly used impact velocities are in the range from
−1 −1
1 ms to 5,5 ms .
NOTE 1 Impact velocities for pendulum or falling weight testing machines can vary by adjusting the striker
release height.
NOTE 2 The reduced impact velocity, v , can be determined as follows: release the pendulum from the
0
appropriately reduced height, without a specimen on the supports. Read the energy KV (in J) indicated by the
0
pointer on the analogue scale. From this, the reduced impact velocity is calculated for a 300 J pendulum as:
300−KV
0
vv= (3)
00s
300
where v is the impact velocity corresponding to the maximum potential energy of the pendulum
0s
(machine capacity), in this case 300 J. If the pendulum maximum available energy is different from
300 J, replace 300 in Formula (3) with the actual maximum available energy. A reduced velocity (1 m/s
to 2 m/s) can be advantageous, particularly in case of brittle behaviour, as it reduces the effect of
oscillations by lowering their relative amplitude and by increasing their number within the time to
fracture t (see 8.2).
f
7.3 Time to fracture
When the time t to initiate unstable fracture is less than 3τ, with τ being the period of force oscillation,
f
fracture occurs after less than three oscillations in the force-time or force-displacement record. In this
case, the instant of crack initiation is not detectable in the force signal with adequate accuracy due to
[4][5][6]
the force oscillations (see Figure 1, type I) and the test cannot be evaluated in accordance with
this International Standard. Reducing the test impact velocity is recommended for further testing in
order to increase the number of oscillations preceding fracture.
NOTE Dynamic evaluation methods have been proposed for determining t independently of force
f
measurements, when time to fracture t < 3τ. Examples are the impact response curve method and the crack tip
f
strain gauge method described in Annex C.
7.4 Multiple specimen tests
To determine dynamic J -R curves by multi-specimen techniques, the fracture process is interrupted at
d
a certain stable crack extension Δa and the process is repeated until an adequate number of data points
are available to define the J -R curve. This procedure is described in Annex D.
d
7.5 Single-specimen tests
Several single-specimen techniques have been proposed in the literature to estimate dynamic
J -R curves. However, only the normalization method described in Annex E is supported by this
d
International Standard.
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ISO 26843:2015(E)

7.6 Post-test crack length measurements
After a test has been performed, the specimen shall be broken open, if necessary, and the fracture
surfaces shall be examined to determine the initial crack length a and the amount of stable crack
0
extension Δa (if applicable). The measurement of initial crack length and stable or unstable crack
extension (if applicable) shall be performed in accordance with ISO 12135 (nine-point average method).
NOTE 1 For some tests, it may be necessary to mark the extent of stable crack extension before opening the
specimen. Stable crack extension may be marked by heat tinting or by post-test fatiguing. Care is to be taken
to minimize post-test deformation. Cooling materials which exhibit a ductile-to-brittle transition may help to
ensure brittle behaviour during specimen opening.
NOTE 2 In the case of poor contrast between fatigue crack, stable crack, and brittle crack after heat tinting,
when using a microscope for crack length measurement, the use of dark field illumination and/or filters may
be beneficial. Digitizing the fracture surface and subsequently evaluating the digital image by image analysis
software may be
...