1、Designation: E1820 15a1E1820 16Standard Test Method forMeasurement of Fracture Toughness1This standard is issued under the fixed designation E1820; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A number
2、 in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1 NOTEA15.2.8 was editorially corrected in November 2016.1. Scope1.1 This test method covers procedures and guidelines for the determination of fracture
3、toughness of metallic materials usingthe following parameters: K, J, and CTOD (). Toughness can be measured in the R-curve format or as a point value. The fracturetoughness determined in accordance with this test method is for the opening mode (Mode I) of loading.NOTE 1Until this version, KIc could
4、be evaluated using this test method as well as by using Test Method E399. To avoid duplication, the evaluationof KIc has been removed from this test method and the user is referred to Test Method E399.1.2 The recommended specimens are single-edge bend, SE(B), compact, C(T), and disk-shaped compact,
5、DC(T). Allspecimens contain notches that are sharpened with fatigue cracks.1.2.1 Specimen dimensional (size) requirements vary according to the fracture toughness analysis applied. The guidelines areestablished through consideration of material toughness, material flow strength, and the individual q
6、ualification requirements ofthe toughness value per values sought.1.3 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only.1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use.
7、It is the responsibilityof the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatorylimitations prior to use.NOTE 2Other standard methods for the determination of fracture toughness using the parameters K, J, and CTOD are contained i
8、nTest Methods E399,E1290, and E1921. This test method was developed to provide a common method for determining all applicable toughness parameters from a single test.2. Referenced Documents2.1 ASTM Standards:2E4 Practices for Force Verification of Testing MachinesE8/E8M Test Methods for Tension Test
9、ing of Metallic MaterialsE21 Test Methods for Elevated Temperature Tension Tests of Metallic MaterialsE23 Test Methods for Notched Bar Impact Testing of Metallic MaterialsE399 Test Method for Linear-Elastic Plane-Strain Fracture Toughness KIc of Metallic MaterialsE1290 Test Method for Crack-Tip Open
10、ing Displacement (CTOD) Fracture Toughness Measurement (Withdrawn 2013)3E1823 Terminology Relating to Fatigue and Fracture TestingE1921 Test Method for Determination of Reference Temperature, To, for Ferritic Steels in the Transition RangeE1942 Guide for Evaluating Data Acquisition Systems Used in C
11、yclic Fatigue and Fracture Mechanics TestingE2298 Test Method for Instrumented Impact Testing of Metallic Materials2.2 ASTM Data Set:4E1820/1DS1(2015) Standard data set to evaluate computer algorithms for evaluation of JIc using, Annex A9 of E18201 This test method is under the jurisdiction of ASTM
12、Committee E08 on Fatigue and Fracture and is the direct responsibility of Subcommittee E08.07 on FractureMechanics.Current edition approved Oct. 15, 2015Dec. 1, 2016. Published November 2015February 2017. Originally approved in 1996. Last previous edition approved in 2015 asE1820 15.E1820 151. DOI:
13、10.1520/E1820-15AE0110.1520/E1820-162 For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at serviceastm.org. For Annual Book of ASTM Standardsvolume information, refer to the standards Document Summary page on the ASTM website.3 The last approved versi
14、on of this historical standard is referenced on www.astm.org.4 This data set is available for download from ASTM at https:/www.astm.org/COMMITTEE/E08.htm, under the heading, Additional Information.This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an i
15、ndication of what changes have been made to the previous version. Becauseit may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current versionof the standard as published by ASTM is to b
16、e considered the official document.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States13. Terminology3.1 Terminology E1823 is applicable to this test method. Only items that are exclusive to Test Method E1820, or that havespecific discuss
17、ion items associated, are listed in this section.3.2 Definitions of Terms Specific to This Standard:3.2.1 compliance LF1, nthe ratio of displacement increment to force increment.3.2.2 crack opening displacement (COD) L, nforce-induced separation vector between two points at a specific gage length.Th
18、e direction of the vector is normal to the crack plane.3.2.2.1 DiscussionIn this practice, displacement, v, is the total displacement measured by clip gages or other devices spanning the crack faces.3.2.3 crack extension, a L, nan increase in crack size.3.2.4 crack-extension force, G FL1 or FLL2, nt
19、he elastic energy per unit of new separation area that is made availableat the front of an ideal crack in an elastic solid during a virtual increment of forward crack extension.3.2.5 crack-tip opening displacement (CTOD), L, ncrack displacement resulting from the total deformation (elastic plusplast
20、ic) at variously defined locations near the original (prior to force application) crack tip.3.2.5.1 DiscussionIn this test method, CTOD is the displacement of the crack surfaces normal to the original (unloaded) crack plane at the tip of thefatigue precrack, ao. In this test method, CTOD is calculat
21、ed at the original crack size, ao, from measurements made from the forceversus displacement record.3.2.5.2 DiscussionIn CTOD testing, Ic L is a value of CTOD near the onset of slow stable crack extension, here defined as occurring at ap = 0.2mm (0.008 in.) + 0.7Ic.3.2.5.3 DiscussionIn CTOD testing,
22、c L is the value of CTOD at the onset of unstable crack extension (see 3.2.38) or pop-in (see 3.2.24) whenap 0.2 mm (0.008 in.) + 0.7u. The u corresponds to the force Pu and the clip gage displacement vu (seeFig. 1). It may be size-dependent and a function of test specimen geometry. It can be useful
23、 to define limits on ductile fracturebehavior.3.2.5.5 DiscussionIn CTOD testing, c* L characterizes the CTOD fracture toughness of materials at fracture instability prior to the onset ofsignificant stable tearing crack extension. The value of c* determined by this test method represents a measure of
24、 fracturetoughness at instability without significant stable crack extension that is independent of in-plane dimensions. However, there maybe a dependence of toughness on thickness (length of crack front).3.2.6 dial energy, KV FLabsorbed energy as indicated by the impact machine encoder or dial indi
25、cator, as applicable.3.2.7 dynamic stress intensity factor, KJdThe dynamic equivalent of the stress intensity factor KJ, calculated from J using theequation specified in this test method.3.2.8 dynamic ultimate tensile strength, TSd FL-2dynamic equivalent of the ultimate tensile strength, measured at
26、 theequivalent strain rate of the fracture toughness test.3.2.9 dynamic yield strength, YSd FL-2dynamic equivalent of the yield strength, measured at the equivalent strain rate ofthe fracture toughness test.3.2.10 effective thickness, Be L , nfor side-grooved specimens Be = B (B BN)2/B. This is used
27、 for the elastic unloadingcompliance measurement of crack size.3.2.11 effective yield strength, Y FL2,nan assumed value of uniaxial yield strength that represents the influence of plasticyielding upon fracture test parameters.3.2.11.1 DiscussionIt is calculated as the average of the 0.2 % offset yie
28、ld strength YS, and the ultimate tensile strength, TS as follows:Y 5 YS1TS2 (1)3.2.11.2 DiscussionIn estimating Y, influences of testing conditions, such as loading rate and temperature, should be considered.3.2.11.3 DiscussionThe dynamic effective yield strength, Yd, is the dynamic equivalent of th
29、e effective yield strength, and is calculated as the averageof the dynamic yield strength and dynamic ultimate tensile strength.3.2.12 general yield force, Pgy Fin an instrumented impact test, applied force corresponding to general yielding of thespecimen ligament. It corresponds to Fgy, as used in
30、Test Method E2298.3.2.13 J-integral, J FL1, na mathematical expression, a line or surface integral that encloses the crack front from one cracksurface to the other, used to characterize the local stress-strain field around the crack front.3.2.13.1 DiscussionThe J-integral expression for a two-dimens
31、ional crack, in the x-z plane with the crack front parallel to the z-axis, is the line integralas follows:J 5* SWdy2Tux dsD (2)where:W = loading work per unit volume or, for elastic bodies, strain energy density, = path of the integral, that encloses (that is, contains) the crack tip,E1820 163ds = i
32、ncrement of the contour path,T = outward traction vector on ds,u = displacement vector at ds,x, y, z = rectangular coordinates, andTux ds = rate of work input from the stress field into the area enclosed by .3.2.13.2 DiscussionThe value of J obtained from this equation is taken to be path-independen
33、t in test specimens commonly used, but in servicecomponents (and perhaps in test specimens) caution is needed to adequately consider loading interior to such as from rapidmotion of the crack or the service component, and from residual or thermal stress.3.2.13.3 DiscussionIn elastic (linear or nonlin
34、ear) solids, the J-integral equals the crack-extension force, G. (See crack extension force.)3.2.13.4 DiscussionIn elastic (linear and nonlinear) solids for which the mathematical expression is path independent, the J-integral is equal to thevalue obtained from two identical bodies with infinitesima
35、lly differing crack areas each subject to stress. The parameter J is thedifference in work per unit difference in crack area at a fixed value of displacement or, where appropriate, at a fixed value of force(1)5.3.2.13.5 DiscussionThe dynamic equivalent of Jc isJcd,X, with X = order of magnitude of J
36、-integral rate.3.2.14 Jc FL1 The property Jc determined by this test method characterizes the fracture toughness of materials at fractureinstability prior to the onset of significant stable tearing crack extension. The value of Jc determined by this test method representsa measure of fracture toughn
37、ess at instability without significant stable crack extension that is independent of in-plane dimensions;however, there may be a dependence of toughness on thickness (length of crack front).3.2.15 Ju FL1The quantity Ju determined by this test method measures fracture instability after the onset of s
38、ignificantstable tearing crack extension. It may be size-dependent and a function of test specimen geometry. It can be useful to define limitson ductile fracture behavior.3.2.15.1 DiscussionThe dynamic equivalent of Ju is Jud,X, with X = order of magnitude of J-integral rate.3.2.16 J-integral rate,
39、J FL21T21#derivative of J with respect to time.3.2.17 machine capacity, MC FLmaximum available energy of the impact testing machine.3.2.18 maximum force, Pmax Fin an instrumented impact test, maximum value of applied force. It corresponds to Fm, asused in Test Method E2298.3.2.19 net thickness, BN L
40、,ndistance between the roots of the side grooves in side-grooved specimens.3.2.20 original crack size, ao L , nthe physical crack size at the start of testing.3.2.20.1 DiscussionIn this test method, aoq is used to denote original crack size estimated from compliance.3.2.21 original remaining ligamen
41、t, bo L,ndistance from the original crack front to the back edge of the specimen, that is(bo = W ao).5 The boldface numbers in parentheses refer to the list of references at the end of this standard.E1820 1643.2.22 physical crack size, ap L , nthe distance from a reference plane to the observed crac
42、k front. This distance mayrepresent an average of several measurements along the crack front. The reference plane depends on the specimen form, and it isnormally taken to be either the boundary, or a plane containing either the load-line or the centerline of a specimen or plate. Thereference plane i
43、s defined prior to specimen deformation.3.2.23 plane-strain fracture toughness, JIc FL1, KJIc FL3/2 , nthe crack-extension resistance under conditions ofcrack-tip plane-strain.3.2.23.1 DiscussionFor example, in Mode I for slow rates of loading and substantial plastic deformation, plane-strain fractu
44、re toughness is the valueof the J-integral designated JIc FL1 as measured using the operational procedure (and satisfying all of the qualificationrequirements) specified in this test method, that provides for the measurement of crack-extension resistance near the onset of stablecrack extension.3.2.2
45、3.2 DiscussionFor example, in Mode I for slow rates of loading, plane-strain fracture toughness is the value of the stress intensity designated KJIccalculated from JIc using the equation (and satisfying all of the qualification requirements) specified in this test method, thatprovides for the measur
46、ement of crack-extension resistance near the onset of stable crack extension under dominant elasticconditions (2).3.2.23.3 DiscussionThe dynamic equivalent of JIc is JIcd,X , with X = order of magnitude of J-integral rate.3.2.24 pop-in, na discontinuity in the force versus clip gage displacement rec
47、ord. The record of a pop-in shows a suddenincrease in displacement and, generally a decrease in force. Subsequently, the displacement and force increase to above theirrespective values at pop-in.3.2.25 R-curve or J-R curve, na plot of crack extension resistance as a function of stable crack extensio
48、n, ap or ae.3.2.25.1 DiscussionIn this test method, the J-R curve is a plot of the far-field J-integral versus the physical crack extension, ap. It is recognized thatthe far-field value of J may not represent the stress-strain field local to a growing crack.3.2.26 remaining ligament, b L, ndistance
49、from the physical crack front to the back edge of the specimen, that is(b = W ap).3.2.27 specimen center of pin hole distance, H* L, nthe distance between the center of the pin holes on a pin-loadedspecimen.3.2.28 specimen gage length, d L, nthe distance between the points of displacement measure (for example, clip gage, gagelength).3.2.29 specimen span, S L, nthe distance between specimen suppo
