astm e399 standard development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ analysis methodย ยท โ€ข theastm e399...

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ASTM E399 Standard Development โ€“ Analysis Method William G. Tilson, Jacobs Space Exploration Group

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Page 1: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

ASTM E399 Standard Development โ€“ ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis

MethodWilliam G. Tilson, Jacobs Space Exploration Group

Page 2: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Background

โ€ข The ASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ๐ผ๐ผ๐ผ๐ผ, for metallic materials.

โ€ข The test consists of monotonically loading a pre-cracked test specimen to failure while recording the applied load and the crack mouth opening displacement.

0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1

Crack Mouth Opening Displacement (in)

0

500

1000

1500

2000

2500

3000

3500

4000

Load

(lbs

)

Example Test Setup Example Test Record 2

Page 3: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Background

โ€ข Several test specimen types are allowable per ASTM E399; two common geometries are the compact tension (C(T)) and the single-edge bend (SE(B)) geometries.

B: thicknessBn: side groove thicknessW: widtha: crack lengthbo: ligament (W-a)

3

Page 4: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Background

โ€ข The test result is an estimate of the plane-strain fracture toughness, ๐พ๐พ๐‘ž๐‘ž, determined by the intercept of the test record with a 95% secant-offset construction line.

0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1

COD (in)

0

500

1000

1500

2000

2500

3000

3500

4000

Forc

e (lb

f)

Kq = 39.6 ksi โˆš (in)

Pm/Pq = 1.37

Curve Fit

Offset Secant Line

Pq (E399)โ€ข The 95% offset represents

crack extension corresponding to ~2% of the original specimen ligament (assuming that all compliance change is the result of crack extension)

โ€ข If the test meets certain validity requirements based on specimen size and test behavior, the result is valid, and ๐พ๐พ๐‘ž๐‘ž =๐พ๐พ๐ผ๐ผ๐ผ๐ผ

4

Page 5: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Background

โ€ข In 2005, Wallin presented evidence that test results for specimens that exhibit Type I behavior (rising R curve, as shown in the previous example test records) are biased by ligament size.

Wallin, K. R. W. โ€œCritical Assessment of the Standard ASTM E 399,โ€ Journal of ASTM International, vol. 2, no. 4, pp. 1-21, 20055

Page 6: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Method

โ€ข Wallin proposed an alternative analysis method, ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ, as a size-insensitive fracture toughness parameter, which was later refined by James, et al.

P

CMOD

Initial compliance

โ€ข The offset parameter is a function of ligament size (in mm):

ฮ”๐ถ๐ถ๐ผ๐ผ๐ผ๐ผ =135

(๐‘Š๐‘Š โˆ’ ๐‘Ž๐‘Ž)โ€ข Corresponds to a fixed crack extension

of 0.5 mm.

โ€ข Fixed allowable plastic zone size (in mm).

๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ๐œŽ๐œŽ๐‘Œ๐‘Œ๐‘Œ๐‘Œ

2

< 12.5

Offset compliance, large (๐‘Š๐‘Šโˆ’ ๐‘Ž๐‘Ž)

Offset compliance, small (๐‘Š๐‘Šโˆ’ ๐‘Ž๐‘Ž)

6

Post-PmaxKIsi?

Page 7: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Method

โ€ข Analysis performed by James, et. al. confirmed that:

โ€ข Limitations on plastic zone size ensure crack extension.

โ€ข Linear-elastic fracture mechanics assumptions are maintained by the alternative approach.

โ€ข Define a ligament limit factor, ๐‘€๐‘€๐พ๐พ, where

M. James, D. Wells, P. Allen and K. Wallin, "A Review of the Proposed KIsi Offset-Secant Method for Size-Insensitive Linear Elastic Fracture Toughness Evaluation," 17th International ASTM/ESIS Symposium on Fatigue and Fracture Mechanics, 2017.

๐‘€๐‘€๐พ๐พ = ๐‘๐‘0๐œŽ๐œŽ๐‘ฆ๐‘ฆ๐ผ๐ผ๐พ๐พ

2

โ€ข For E399, ๐‘€๐‘€๐พ๐พ=2.5. For KIsi, ๐‘€๐‘€๐พ๐พ = ๐‘๐‘0/12.5 mm

7

Page 8: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Experimental Validation

โ€ข The ongoing study attempts to validate the assumptions of the ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ analysis method

โ€ข Are size dependent effects removed when compared to the typical E399 analysis?

โ€ข How accurate is the assumption that the variable secant offset corresponds to 0.5mm crack extension, given plasticity and experimental uncertainties?

โ€ข Do the limits on plastic zone size ensure crack extension?

8

Page 9: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Test Specimens

โ€ข Test specimens were obtained from a plate of 7475-T7351 aluminum.โ€ข Tensile specimens were obtained in the three main directions (L, T,

ST).โ€ข Fracture specimens

were machined in the L-T direction.

โ€ข Details of the cut plan can be found in CP-544.

9

Page 10: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Test Matrix - Tensile Tests

โ€ข Four samples were tested at each orientation (L, T, and ST)โ€ข Average results are shown below.

Average

OrientationUltimate

Strength (MPa)Yield Strength

(MPa)Fracture

Elongation (%)L 476 401 16.9T 482 407 13.8

ST 476 390 10.2

10

Page 11: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

โ€ข All specimens have L-T orientation.โ€ข Several spares for each specimen configuration are available for

additional testing.

Test Matrix โ€“ Fracture Tests

Specimen Dimensions (mm) Number of TestsE399

E1820Interrupted

W B W/B Plane-sided Side grooved Plane-sided Side grooved25.4 6.35 4 2 1 2 2 1 Completed25.4 12.7 2 2 1 2 2 138.1 9.525 4 2 1 2 2 138.1 19.05 2 2 1 2 2 150.8 12.7 4 2 1 2 2 150.8 25.4 2 2 1 2 2 176.2 19.05 4 2 1 2 2 176.2 38.1 2 2 1 2 2 1

11

Page 12: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Slope Fitting

โ€ข Slope determination for the purposes of determining the ๐พ๐พ๐ผ๐ผ๐ผ๐ผ and ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผpoints is done by using the Slope Determination through Analysis of Residuals (SDAR) method, developed by Graham and Adler.

โ€ข The SDAR algorithm provides an objective and repeatable method for slope determination.

S. M. Graham and M. A. Adler, โ€œDetermining the Slope and Quality of Fit for the Linear Part of a Test Record," Journal of Testing and Evaluation, Vol. 39, No. 2, 2011.

-0.16 -0.14 -0.12 -0.1 -0.08 -0.06 -0.04 -0.02 0 0.02

Reduced Displacement (mm)

1

2

3

4

5

6

7

8

9

Forc

e (k

N)

โ€ข The response of this alloy is such that the initial linear region is small; results are sensitive to changes in fit.

12

Page 13: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K Results

โ€ข Results obtained thus far from four specimen configurations.โ€ข In general, the ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ results are more consistent than the E399 ๐พ๐พ๐ผ๐ผ๐ผ๐ผ results. Data shown includes results from interrupted tests, if applicable.

0 5 10 15 20 25 30 35 40 45 50 55

W-a (mm)

0

10

20

30

40

50

60

Kq

(MPa

โˆš(m

))

E399: bo

> 2.5(KQ

/YS )

2

KIsi

: (KQ

/YS )

2 <12.5mm

W = 25.4, B = 12.7 (KIc)

W = 25.4, B = 12.7 (KIsi)

W = 38.1, B = 9.525 (KIc)

W = 38.1, B = 9.525 (KIsi)

W = 50.8, B = 25.4 (KIc)

W = 50.8, B = 25.4 (KIsi)

W = 50.8, B = 12.7 (KIc)

W = 50.8, B = 12.7 (KIsi)

13

Page 14: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Interrupted Tests

โ€ข Goal is to validate that the ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ point corresponds to 0.5 mm of crack extension.

โ€ข Samples will be precracked as close as possible to the lengths of the standard E399 tests using compliance crack monitoring techniques.

โ€ข E399 test will be conducted, but halted at the CMOD corresponding to the ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ point from the E399 tests.

โ€ข Specimens will be chemically stained in order to determine the amount of crack extension.

P

CMOD

P

CMOD

E399 Test Interrupted Test

๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผpoint

CMOD for ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ

Stop and unload at CMOD for ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ

14

Page 15: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Interrupted Testsโ€ข Specimens are marked with a 10% sodium hydroxide solution. During

marking, specimens are loaded between 50% and 80% of the final test load.

โ€ข Crack extension measurements were obtained using a Keyence VR-3200 3D measurement microscope.

โ€ข The current approach is to determine crack extension by the crack measurement method of E399; there has been limited crack extension at specimen edges, so only the middle three measurements are averaged.

15

Page 16: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Interrupted Tests - Results

โ€ข In general, the ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ point has tended to underestimate the desired 0.5 mm of crack extension. Some apparent compliance change corresponding to the ๐พ๐พ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ point is expected to be the result of plasticity, so some crack extension less than the target is expected.

โ€ข Future analysis will compare the measured crack extension with the predicted crack extension due to compliance change for the test.

Specimen W (mm) B (mm) MK,limit MK @ KIsi KIsi โˆ†a (mm)

K-1-2-1 25.4 12.7 0.98 0.96 45.2 0.23

K-1-2-4 25.4 12.7 0.99 1.01 44.1 0.15

K-15-2-2 38.1 19.0 1.42 1.45 44.2 0.35

K-15-2-8 38.1 19.0 1.41 1.41 44.8 0.24

K-2-2-1 50.8 25.4 1.96 1.88 45.6 0.41

K-2-2-8 50.9 25.4 1.98 1.90 45.6 0.41

K-2-4-6 50.8 12.6 1.98 2.18 42.6 0.50

K-2-4-8 50.8 12.6 1.99 2.12 43.2 0.2816

Page 17: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

Detailed Results

17

Page 18: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

1

2

3

4

5

6

7

8

9

10

Forc

e (k

N)

Kq = 35.0 MPa โˆš (m)

Pm/Pq = 1.35

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

1

2

3

4

5

6

7

8

9

10

Forc

e (k

N)

Kq = 44.4 MPa โˆš (m)

Pm/Pq = 1.07

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 25.4 mm B = 12.7 mm Bn = 12.7 mm a = 13.2 mm MK,limit (KIsi) = 0.98

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 6.916 35.0 1.35 1.60 Pmax/Pq, Ligament

KIsi 8.753 44.4 1.07 1.00 Valid

K-1-2-2 - E399 Test

Page 19: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.2 0.4 0.6 0.8 1

COD (mm)

0

1

2

3

4

5

6

7

8

9

10

Forc

e (k

N)

Kq = 39.8 MPa โˆš (m)

Pm/Pq = 1.19

Curve Fit

Offset Secant Line

Pq (E399)

0 0.2 0.4 0.6 0.8 1

COD (mm)

0

1

2

3

4

5

6

7

8

9

10

Forc

e (k

N)

Kq = 46.6 MPa โˆš (m)

Pm/Pq = 1.02

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 25.4 mm B = 12.7 mm Bn = 12.7 mm a = 13.2 mm Mk,limit (KIsi) = 0.98

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 7.867 39.8 1.19 1.23 Pmax/Pq, Ligament

KIsi 9.204 46.6 1.02 0.90 Ligament

K-1-2-9 - E399 Test

Page 20: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.2 0.4 0.6 0.8 1 1.2 1.4

COD (mm)

0

1

2

3

4

5

6

7

8

Forc

e (k

N)

Kq = 33.6 MPa โˆš (m)

Pm/Pq = 1.35

Curve Fit

Offset Secant Line

Pq (E399)

0 0.2 0.4 0.6 0.8 1 1.2 1.4

COD (mm)

0

1

2

3

4

5

6

7

8

Forc

e (k

N)

Kq = 44.6 MPa โˆš (m)

Pm/Pq = 1.02

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 25.4 mm B = 12.7 mm Bn = 10.2 mm a = 13.3 mm Mk,limit (KIsi) = 0.97

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 5.893 33.6 1.35 1.73 Pmax/Pq, Ligament

KIsi 7.831 44.6 1.02 0.98 Valid

K-1-2-8 - E399 Test (Side Grooved)

Page 21: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6

COD (mm)

0

1

2

3

4

5

6

7

8

9

Forc

e (k

N)

Kq = 35.5 MPa โˆš (m)

Pm/Pq = 1.28

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6

COD (mm)

0

1

2

3

4

5

6

7

8

9

Forc

e (k

N)

Kq = 45.2 MPa โˆš (m)

Pm/Pq = 1.00

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 25.4 mm B = 12.7 mm Bn = 12.7 mm a = 13.1 mm Mk,limit (KIsi) = 0.98

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig. Validity

KIc 7.041 35.5 --- 1.56 Not Valid

KIsi 8.971 45.2 --- 0.96 Not Valid

K-1-2-1 - Interrupted Test

Page 22: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-1-2-1 โ€“ Fracture Surface

22

Average crack extension: 0.23 mm

Page 23: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6

COD (mm)

0

1

2

3

4

5

6

7

8

9

Forc

e (k

N)

Kq = 35.6 MPa โˆš (m)

Pm/Pq = 1.24

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6

COD (mm)

0

1

2

3

4

5

6

7

8

9

Forc

e (k

N)

Kq = 44.1 MPa โˆš (m)

Pm/Pq = 1.00

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 25.4 mm B = 12.7 mm Bn = 12.7 mm a = 13.1 mm Mk,limit (KIsi) = 0.99

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig. Validity

KIc 7.095 35.6 --- 1.56 Not Valid

KIsi 8.795 44.1 --- 1.01 Valid

K-1-2-4 - Interrupted Test

Page 24: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-1-2-4 โ€“ Fracture Surface

Average crack extension: 0.15 mm

24

Page 25: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 40.5 MPa โˆš (m)

Pm/Pq = 1.19

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 44.1 MPa โˆš (m)

Pm/Pq = 1.09

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 38.1 mm B = 19.0 mm Bn = 19.0 mm a = 20.6 mm Mk,limit (KIsi) = 1.39

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 13.608 40.5 1.19 1.70 Pmax/Pq, Ligament

KIsi 14.799 44.1 1.09 1.43 Valid

K-15-2-5 - E399 Test

Page 26: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

18

Forc

e (k

N)

Kq = 41.6 MPa โˆš (m)

Pm/Pq = 1.17

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

18

Forc

e (k

N)

Kq = 45.0 MPa โˆš (m)

Pm/Pq = 1.08

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 38.1 mm B = 19.0 mm Bn = 19.0 mm a = 20.4 mm Mk,limit (KIsi) = 1.41

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 14.220 41.6 1.17 1.63 Pmax/Pq, Ligament

KIsi 15.363 45.0 1.08 1.40 Ligament

K-15-2-6 - E399 Test

Page 27: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 40.5 MPa โˆš (m)

Pm/Pq = 1.16

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 44.1 MPa โˆš (m)

Pm/Pq = 1.07

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 38.1 mm B = 19.0 mm Bn = 15.3 mm a = 20.3 mm Mk,limit (KIsi) = 1.42

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 12.562 40.5 1.16 1.74 Pmax/Pq, Ligament

KIsi 13.673 44.1 1.07 1.47 Valid

K-15-2-10 - E399 Test (Side Grooved)

Page 28: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 41.5 MPa โˆš (m)

Pm/Pq = 1.07

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 44.2 MPa โˆš (m)

Pm/Pq = 1.00

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 38.1 mm B = 19.0 mm Bn = 19.0 mm a = 20.4 mm Mk,limit (KIsi) = 1.42

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig. Validity

KIc 14.295 41.5 --- 1.65 Not Valid

KIsi 15.230 44.2 --- 1.45 Valid

K-15-2-2 - Interrupted Test

Page 29: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-15-2-2 โ€“ Fracture Surface

Average crack extension: 0.35 mm

29

Page 30: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 41.6 MPa โˆš (m)

Pm/Pq = 1.08

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8

COD (mm)

0

2

4

6

8

10

12

14

16

Forc

e (k

N)

Kq = 44.8 MPa โˆš (m)

Pm/Pq = 1.00

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 38.1 mm B = 19.0 mm Bn = 19.0 mm a = 20.4 mm Mk,limit (KIsi) = 1.41

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig. Validity

KIc 14.242 41.6 --- 1.63 Not Valid

KIsi 15.324 44.8 --- 1.41 Not Valid

K-15-2-8 - Interrupted Test

Page 31: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-15-2-8 โ€“ Fracture Surface

Average crack extension: 0.24 mm

31

Page 32: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

5

10

15

20

25

30

Forc

e (k

N)

Kq = 45.4 MPa โˆš (m)

Pm/Pq = 1.13

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

5

10

15

20

25

30

Forc

e (k

N)

Kq = 45.8 MPa โˆš (m)

Pm/Pq = 1.12

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.8 mm B = 25.4 mm Bn = 25.4 mm a = 26.5 mm Mk,limit (KIsi) = 1.95

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 25.182 45.4 1.13 1.89 Pmax/Pq, Ligament

KIsi 25.390 45.8 1.12 1.86 Ligament

K-2-2-5 - E399 Test

Page 33: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

5

10

15

20

25

30

Forc

e (k

N)

Kq = 45.3 MPa โˆš (m)

Pm/Pq = 1.16

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

5

10

15

20

25

30

Forc

e (k

N)

Kq = 46.1 MPa โˆš (m)

Pm/Pq = 1.14

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.8 mm B = 25.4 mm Bn = 25.4 mm a = 26.2 mm Mk,limit (KIsi) = 1.97

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 25.547 45.3 1.16 1.92 Pmax/Pq, Ligament

KIsi 25.962 46.1 1.14 1.85 Ligament

K-2-2-10 - E399 Test

Page 34: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9

COD (mm)

0

5

10

15

20

25

Forc

e (k

N)

Kq = 45.4 MPa โˆš (m)

Pm/Pq = 1.03

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9

COD (mm)

0

5

10

15

20

25

Forc

e (k

N)

Kq = 45.6 MPa โˆš (m)

Pm/Pq = 1.03

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.8 mm B = 25.4 mm Bn = 25.4 mm a = 26.3 mm Mk,limit (KIsi) = 1.96

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig. Validity

KIc 25.475 45.4 --- 1.91 Not Valid

KIsi 25.619 45.6 --- 1.88 Not Valid

K-2-2-1 - Interrupted Test

Page 35: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-2-2-1 โ€“ Fracture Surface

Average crack extension: 0.41 mm

35

Page 36: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

COD (mm)

0

5

10

15

20

25

Forc

e (k

N)

Kq = 44.7 MPa โˆš (m)

Pm/Pq = 1.06

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

COD (mm)

0

5

10

15

20

25

Forc

e (k

N)

Kq = 45.6 MPa โˆš (m)

Pm/Pq = 1.04

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.9 mm B = 25.4 mm Bn = 25.4 mm a = 26.2 mm Mk,limit (KIsi) = 1.98

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig. Validity

KIc 25.323 44.7 --- 1.98 Not Valid

KIsi 25.824 45.6 --- 1.90 Not Valid

K-2-2-8 - Interrupted Test

Page 37: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-2-2-8 โ€“ Fracture Surface

Average crack extension: 0.41 mm

37

Page 38: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

18

Forc

e (k

N)

Kq = 43.5 MPa โˆš (m)

Pm/Pq = 1.37

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

18

Forc

e (k

N)

Kq = 44.4 MPa โˆš (m)

Pm/Pq = 1.34

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.8 mm B = 12.6 mm Bn = 12.6 mm a = 25.9 mm MK,limit (KIsi) = 2.00

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 12.512 43.5 1.37 2.11 Pmax/Pq, Ligament

KIsi 12.758 44.4 1.34 2.03 Valid

K-2-4-7 - E399 Test

Page 39: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

18

Forc

e (k

N)

Kq = 47.6 MPa โˆš (m)

Pm/Pq = 1.24

Curve Fit

Offset Secant Line

Pq (E399)

0 0.5 1 1.5 2 2.5

COD (mm)

0

2

4

6

8

10

12

14

16

18

Forc

e (k

N)

Kq = 48.2 MPa โˆš (m)

Pm/Pq = 1.22

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.8 mm B = 12.6 mm Bn = 12.6 mm a = 25.9 mm Mk,limit (KIsi) = 1.99

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 13.640 47.6 1.24 1.76 Pmax/Pq, Ligament

KIsi 13.809 48.2 1.22 1.72 Ligament

K-2-4-10 - E399 Test

Page 40: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8

COD (mm)

0

2

4

6

8

10

12

14

Forc

e (k

N)

Kq = 43.7 MPa โˆš (m)

Pm/Pq = 1.15

Curve Fit

Offset Secant Line

Pq (E399)

0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8

COD (mm)

0

2

4

6

8

10

12

14

Forc

e (k

N)

Kq = 44.7 MPa โˆš (m)

Pm/Pq = 1.12

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.9 mm B = 12.7 mm Bn = 10.1 mm a = 26.0 mm Mk,limit (KIsi) = 1.99

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Validity

KIc 11.152 43.7 1.15 2.08 Pmax/Pq, Ligament

KIsi 11.392 44.7 1.12 1.99 Valid

K-2-4-4 - E399 Test (Side Grooved)

Page 41: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9

COD (mm)

0

2

4

6

8

10

12

Forc

e (k

N)

Kq = 41.9 MPa โˆš (m)

Pm/Pq = 1.07

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9

COD (mm)

0

2

4

6

8

10

12

Forc

e (k

N)

Kq = 42.6 MPa โˆš (m)

Pm/Pq = 1.06

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.8 mm B = 12.6 mm Bn = 12.6 mm a = 26.1 mm Mk,limit (KIsi) = 1.98

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig.Validity

KIc 11.833 41.9 --- 2.25 Not Valid

KIsi 12.021 42.6 --- 2.18 Valid

K-2-4-6 - Interrupted Test

Page 42: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-2-4-6 โ€“ Fracture Surface

Average crack extension: 0.50 mm

42

Page 43: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

KIc Method KIsi Method

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9

COD (mm)

0

2

4

6

8

10

12

Forc

e (k

N)

Kq = 42.7 MPa โˆš (m)

Pm/Pq = 1.04

Curve Fit

Offset Secant Line

Pq (E399)

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9

COD (mm)

0

2

4

6

8

10

12

Forc

e (k

N)

Kq = 43.2 MPa โˆš (m)

Pm/Pq = 1.03

Curve Fit

Offset Secant Line

Pq (KIsi)

W = 50.8 mm B = 12.6 mm Bn = 12.6 mm a = 26.0 mm MK,limit (KIsi) = 1.99

Pq (kN) Kq(MPaโˆšm)

Pmax/Pq MK @ Kq Lig. Validity

KIc 12.150 42.7 --- 2.18 Not Valid

KIsi 12.316 43.2 --- 2.12 Valid

K-2-4-8 - Interrupted Test

Page 44: ASTM E399 Standard Development โ€“ ๐ผ๐ผ๐ผ๐ผ๐ผ๐ผ Analysis Methodย ยท โ€ข TheASTM E399 test method is used to determine the plane-strain fracture toughness, ๐พ๐พ ๐ผ๐ผ๐ผ๐ผ,

K-2-4-8 โ€“ Fracture Surface

Average crack extension: 0.28 mm

44