ASTM E1921-2018a Standard Test Method for Determination of Reference Temperature To for Ferritic Steels in the Transition Range.pdf

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1、Designation: E1921 18aStandard Test Method forDetermination of Reference Temperature, To, for FerriticSteels in the Transition Range1This standard is issued under the fixed designation E1921; the number immediately following the designation indicates the year oforiginal adoption or, in the case of r

2、evision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.1. Scope1.1 This test method covers the determination of a referencetemperature, To, which characterizes the

3、fracture toughness offerritic steels that experience onset of cleavage cracking atelastic, or elastic-plastic KJcinstabilities, or both. The specifictypes of ferritic steels (3.2.1) covered are those with yieldstrengths ranging from 275 to 825 MPa (40 to 120 ksi) andweld metals, after stress-relief

4、annealing, that have 10 % orless strength mismatch relative to that of the base metal.1.2 The specimens covered are fatigue precracked single-edge notched bend bars, SE(B), and standard or disk-shapedcompact tension specimens, C(T) or DC(T). A range ofspecimen sizes with proportional dimensions is r

5、ecommended.The dimension on which the proportionality is based isspecimen thickness.1.3 Median KJcvalues tend to vary with the specimen typeat a given test temperature, presumably due to constraintdifferences among the allowable test specimens in 1.2. Thedegree of KJcvariability among specimen types

6、 is analyticallypredicted to be a function of the material flow properties (1)2and decreases with increasing strain hardening capacity for agiven yield strength material. This KJcdependency ultimatelyleads to discrepancies in calculated Tovalues as a function ofspecimen type for the same material. T

7、ovalues obtained fromC(T) specimens are expected to be higher than Tovaluesobtained from SE(B) specimens. Best estimate comparisons ofseveral materials indicate that the average difference betweenC(T) and SE(B)-derived Tovalues is approximately 10C (2).C(T) and SE(B) Todifferences up to 15C have als

8、o beenrecorded (3). However, comparisons of individual, small data-sets may not necessarily reveal this average trend. Datasetswhich contain both C(T) and SE(B) specimens may generateToresults which fall between the Tovalues calculated usingsolely C(T) or SE(B) specimens. It is therefore stronglyrec

9、ommended that the specimen type be reported along withthe derived Tovalue in all reporting, analysis, and discussion ofresults. This recommended reporting is in addition to therequirements in 11.1.1.1.4 Requirements are set on specimen size and the numberof replicate tests that are needed to establi

10、sh acceptablecharacterization of KJcdata populations.1.5 Tois dependent on loading rate. Tois evaluated for aquasi-static loading rate range with 0.12MPam/s) in Annex A1. Note that this threshold loading ratefor application of Annex A1 is a much lower threshold than isrequired in other fracture toug

11、hness test methods such as E399and E1820.1.6 The statistical effects of specimen size on KJcin thetransition range are treated using the weakest-link theory (4)applied to a three-parameter Weibull distribution of fracturetoughness values. A limit on KJcvalues, relative to thespecimen size, is specif

12、ied to ensure high constraint conditionsalong the crack front at fracture. For some materials, particu-larly those with low strain hardening, this limit may not besufficient to ensure that a single-parameter (KJc) adequatelydescribes the crack-front deformation state (5).1.7 Statistical methods are

13、employed to predict the transi-tion toughness curve and specified tolerance bounds for 1Tspecimens of the material tested. The standard deviation of thedata distribution is a function of Weibull slope and median KJc.The procedure for applying this information to the establish-ment of transition temp

14、erature shift determinations and theestablishment of tolerance limits is prescribed.1.8 The procedures described in this test method assumethat the data set represents a macroscopically homogeneousmaterial, such that the test material has uniform tensile andtoughness properties. Application of this

15、test method to aninhomogeneous material will result in an inaccurate estimate ofthe transition reference value Toand nonconservative confi-dence bounds. For example, multi-pass weldments can createheat-affected and brittle zones with localized properties that are1This test method is under the jurisd

16、iction of ASTM Committee E08 on Fatigueand Fracture and is the direct responsibility of E08.07 on Fracture Mechanics.Current edition approved June 1, 2018. Published October 2018. Originallyapproved in 1997. Last previous edition approved in 2018 as E1921 18. DOI:10.1520/E1921-18A.2The boldface numb

17、ers in parentheses refer to the list of references at the end ofthis standard.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United StatesThis international standard was developed in accordance with internationally recognized principles on standar

18、dization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.1quite different from either the bulk or weld materials. Thick-section steels also often exh

19、ibit some variation in propertiesnear the surfaces. Metallography and initial screening may benecessary to verify the applicability of these and similarlygraded materials. Section 10.6 provides a screening criterion toassess whether the data set may not be representative of amacroscopically homogene

20、ous material, and therefore, maynot be amenable to the statistical analysis procedures employedin this test method. If the data set fails the screening criterionin 10.6, the homogeneity of the material and its fracturetoughness can be more accurately assessed using the analysismethods described in A

21、ppendix X5.1.9 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety, health, and environmental practices and deter-mine the applicability of regulatory limitations p

22、rior to use.1.10 This international standard was developed in accor-dance with internationally recognized principles on standard-ization established in the Decision on Principles for theDevelopment of International Standards, Guides and Recom-mendations issued by the World Trade Organization Technic

23、alBarriers to Trade (TBT) Committee.2. Referenced Documents2.1 ASTM Standards:3E4 Practices for Force Verification of Testing MachinesE8/E8M Test Methods for Tension Testing of Metallic Ma-terialsE23 Test Methods for Notched Bar Impact Testing of Me-tallic MaterialsE74 Practices for Calibration and

24、Verification for Force-Measuring InstrumentsE111 Test Method for Youngs Modulus, Tangent Modulus,and Chord ModulusE177 Practice for Use of the Terms Precision and Bias inASTM Test MethodsE208 Test Method for Conducting Drop-Weight Test toDetermine Nil-Ductility Transition Temperature of Fer-ritic St

25、eelsE399 Test Method for Linear-Elastic Plan-Strain FractureToughness KIcof Metallic MaterialsE436 Test Method for Drop-Weight Tear Tests of FerriticSteelsE561 Test Method for KRCurve DeterminationE691 Practice for Conducting an Interlaboratory Study toDetermine the Precision of a Test MethodE1820 T

26、est Method for Measurement of Fracture ToughnessE1823 Terminology Relating to Fatigue and Fracture Testing2.2 ASME Standards:4ASME Boiler and Pressure Vessel Code, Section II, Part D3. Terminology3.1 Terminology given in Terminology E1823 is applicableto this test method.3.2 Definitions:3.2.1 ferrit

27、ic steelstypically carbon, low-alloy, and higheralloy grades. Typical microstructures are bainite, temperedbainite, tempered martensite, and ferrite and pearlite. Allferritic steels have body centered cubic crystal structures thatdisplay ductile-to-cleavage transition temperature fracturetoughness c

28、haracteristics. See also Test Methods E23, E208and E436.3.2.1.1 DiscussionThis definition is not intended to implythat all of the many possible types of ferritic steels have beenverified as being amenable to analysis by this test method.3.2.2 stress-intensity factor, K FL 3/2the magnitude ofthe math

29、ematically ideal crack-tip stress field coefficient (stressfield singularity) for a particular mode of crack-tip regiondeformation in a homogeneous body.3.2.2.1 DiscussionIn this test method, Mode I is assumed.See Terminology E1823 for further discussion.3.2.3 J-integral, J FL1a mathematical express

30、ion; aline or surface integral that encloses the crack front from onecrack surface to the other; used to characterize the localstress-strain field around the crack front (6). See TerminologyE1823 for further discussion.3.3 Definitions of Terms Specific to This Standard:3.3.1 control force, PmFa calc

31、ulated value of maximumforce, used in 7.8.1 to stipulate allowable precracking limits.3.3.2 crack initiationdescribes the onset of crack propa-gation from a preexisting macroscopic crack created in thespecimen by a stipulated procedure.3.3.3 effective modulus, EeffFL2an elastic modulus thatallows a

32、theoretical (modulus normalized) compliance tomatch an experimentally measured compliance for an actualinitial crack size, ao.3.3.4 effective yield strength, YFL-2 an assumed valueof uniaxial yield strength that represents the influence of plasticyielding upon fracture test parameters.3.3.4.1 Discus

33、sionIt is calculated as the average of the0.2 % offset yield strength YS, and the ultimate tensilestrength, TSas follows:Y5YS1TS23.3.5 elastic modulus, E FL2a linear-elastic factorrelating stress to strain, the value of which is dependent on thedegree of constraint. For plane stress, E = E is used,

34、and forplane strain, E/(1 v2) is used, with E being Youngs modulusand v being Poissons ratio.3.3.6 elastic plastic JcFL1J-integral at the onset ofcleavage fracture.3.3.7 elastic-plastic KJFL3/2An elastic-plastic equiva-lent stress intensity factor derived from the J-integral.3.3.7.1 DiscussionIn thi

35、s test method, KJalso implies a3For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.4Available from American Socie

36、ty of Mechanical Engineers (ASME), ASMEInternational Headquarters, Two Park Ave., New York, NY 10016-5990, http:/www.asme.org.E1921 18a2stress intensity factor determined at the test termination pointunder conditions that require censoring the data by 8.9.2.3.3.8 elastic-plastic KJcFL3/2an elastic-p

37、lastic equiva-lent stress intensity factor derived from the J-integral at thepoint of onset of cleavage fracture, Jc.3.3.9 equivalent value of median toughness, KJcmed!eqFL-3/2an equivalent value of the median toughness for amulti-temperature data set.3.3.10 Eta ()a dimensionless parameter that rela

38、tes plas-tic work done on a specimen to crack growth resistance definedin terms of deformation theory J-integral (7).3.3.11 failure probability, pfthe probability that a singleselected specimen chosen at random from a population ofspecimens will fail at or before reaching the KJcvalue ofinterest.3.3

39、.12 initial ligament length, boL the distance from theinitial crack tip, ao, to the back face of a specimen.3.3.13 load-line displacement rate,LLLT-1rate of in-crease of specimen load-line displacement.3.3.14 pop-ina discontinuity in a force versus displace-ment test record (8).3.3.14.1 DiscussionA

40、pop-in event is usually audible, andis a sudden cleavage crack initiation event followed by crackarrest. The test record will show increased displacement anddrop in applied force if the test frame is stiff. Subsequently, thetest record may continue on to higher forces and increaseddisplacements.3.3.

41、15 precracked Charpy, PCC, specimenSE(B) speci-men with W = B = 10 mm (0.394 in.).3.3.16 provisional reference temperature, (ToQ) CInterim Tovalue calculated using the standard test methoddescribed herein. ToQis validated as Toin 10.5.3.3.17 reference temperature, ToCThe test temperatureat which the

42、 median of the KJcdistribution from 1T sizespecimens will equal 100 MPam (91.0 ksiin.).3.3.18 SE(B) specimen span, S Lthe distance betweenspecimen supports (See Test Method E1820 Fig. 3).3.3.19 specimen thickness, B Lthe distance between theparallel sides of a test specimen as depicted in Fig. 13.3.

43、3.19.1 DiscussionIn the case of side-groovedspecimens, the net thickness, BN, is the distance between theroots of the side-groove notches.3.3.20 specimen size, nTa code used to define specimendimensions, where n is expressed in multiples of 1 in.3.3.20.1 DiscussionIn this method, specimen proportion

44、-ality is required. For compact specimens and bend bars,specimen thickness B=ninches.3.3.21 temperature, TQCFor KJcvalues that are devel-oped using specimens or test practices, or both, that do notconform to the requirements of this test method, a temperatureat which KJc (med)= 100 MPam is defined a

45、s TQ.TQis not aprovisional value of To.3.3.22 time to control force, tmT,time to Pm.3.3.23 Weibull fitting parameter, K0a scale parameterlocated at the 63.2 % cumulative failure probability level (9).KJc=K0when pf= 0.632.3.3.24 Weibull slope, bwith pfand KJcdata pairs plotted inlinearized Weibull co

46、ordinates obtainable by rearranging Eq18, b is the slope of a line that defines the characteristics of thetypical scatter of KJcdata.3.3.24.1 DiscussionA Weibull slope of 4 is used exclu-sively in this method.3.3.25 yield strength, YSFL2the stress at which amaterial exhibits a specific limiting devi

47、ation from the propor-tionality of stress to strain at the test temperature. Thisdeviation is expressed in terms of strain.3.3.25.1 DiscussionIt is customary to determine yieldstrength by either (1) Offset Method (usually a strain of 0.2 %is specified) or (2) Total-Extension-Under-Force Method (usu-

48、ally a strain of 0.5 % is specified although other values of strainmay be used).3.3.25.2 DiscussionWhenever yield strength is specified,the method of test must be stated along with the percent offsetor total strain under force. The values obtained by the twomethods may differ.4. Summary of Test Meth

49、od4.1 This test method involves the testing of notched andfatigue precracked bend or compact specimens in a tempera-ture range where either cleavage cracking or crack pop-indevelop during the loading of specimens. Crack aspect ratio,a/W, is nominally 0.5. Specimen width in compact specimensis two times the thickness. In bend bars, specimen width can beeither one or two times the thickness.4.2 Force versus displacement across the notch at a speci-fied location is recorded