ASTM E2207-2002 Standard Practice for Strain-Controlled Axial-Torsional Fatigue Testing with Thin-Walled Tubular Specimens《带有薄壁管状样品的应力控制轴向扭曲疲劳检验的标准实施规程》.pdf
《ASTM E2207-2002 Standard Practice for Strain-Controlled Axial-Torsional Fatigue Testing with Thin-Walled Tubular Specimens《带有薄壁管状样品的应力控制轴向扭曲疲劳检验的标准实施规程》.pdf》由会员分享,可在线阅读,更多相关《ASTM E2207-2002 Standard Practice for Strain-Controlled Axial-Torsional Fatigue Testing with Thin-Walled Tubular Specimens《带有薄壁管状样品的应力控制轴向扭曲疲劳检验的标准实施规程》.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: E 2207 02Standard Practice forStrain-Controlled Axial-Torsional Fatigue Testing with Thin-Walled Tubular Specimens1This standard is issued under the fixed designation E 2207; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revis
2、ion, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.1. Scope1.1 The standard deals with strain-controlled, axial, tor-sional, and combined in- and out-of-phase axia
3、l torsionalfatigue testing with thin-walled, circular cross-section, tubularspecimens at isothermal, ambient and elevated temperatures.This standard is limited to symmetric, completely-reversedstrains (zero mean strains) and axial and torsional waveformswith the same frequency in combined axial-tors
4、ional fatiguetesting. This standard is also limited to thin-walled tubularspecimens (machined from homogeneous materials) and doesnot cover testing of either large-scale components or structuralelements.1.2 This standard does not purport to address all of thesafety concerns, if any, associated with
5、its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:E 3 Practice for Preparation of Metallographic Specimens2E 4 Practices
6、 for Force Verification of Testing Machines2E 6 Terminology Relating to Methods of Mechanical Test-ing2E 8 Test Methods for Tension Testing of Metallic Materials2E 9 Test Methods of Compression Testing of Metallic Ma-terials at Room Temperature2E 83 Practice for Verification and Classification of Ex
7、ten-someters2E 111 Test Method for Youngs Modulus, Tangent Modulus,and Chord Modulus2E 112 Test Methods for Determining Average Grain Size2E 143 Test Method for Shear Modulus at Room Tempera-ture2E 209 Practice for Compression Tests of Metallic Materialsat Elevated Temperatures with Conventional or
8、RapidHeating Rates or Strain Rates2E 467 Practice for Verification of Constant Amplitude Dy-namic Forces in an Axial Fatigue Testing System2E 606 Practice for Strain-Controlled Fatigue Testing2E 1012 Practice for Verification of Specimen Alignmentunder Tensile Loading2E 1417 Practice for Liquid Pene
9、trant Examination3E 1444 Practice for Magnetic Particle Examination3E 1823 Terminology Relating to Fatigue and Fracture Test-ing23. Terminology3.1 Definitions:3.1.1 axial strainrefers to engineering axial strain, e, andis defined as change in length divided by the original length(DLg/Lg).3.1.2 shear
10、 strainrefers to engineering shear strain, g,resulting from the application of a torsional moment to acylindrical specimen. Such a torsional shear strain is simpleshear and is defined similar to axial strain with the exceptionthat the shearing displacement, DLsis perpendicular to ratherthan parallel
11、 to the gage length, Lg, that is, g = DLs/Lg(see Fig.1).NOTE 1g= is related to the angles of twist, u and C as follows:g = tan C, where C is the angle of twist along the gage length of thecylindrical specimen. For small angles tan C approaches C and gapproaches C.g =(d/2)u/Lg, where u expressed in r
12、adians is the angle of twist betweenthe planes defining the gage length of the cylindrical specimen and d is thediameter of the cylindrical specimen.NOTE 2DLsis measurable directly as displacement using speciallycalibrated torsional extensometers or as the arc length DLs=(d/2)u, whereu is measured d
13、irectly with a rotary variable differential transformer.3.1.2.1 DiscussionThe shear strain varies linearly throughthe thin wall of the specimen, with the smallest and largestvalues occurring at the inner and outer diameters of thespecimen, respectively. The value of shear strain on the outersurface,
14、 inner surface, and mean diameter of the specimen shallbe reported. The shear strain determined at the outer diameterof the tubular specimen is recommended for strain-controlledtorsional tests, since cracks typically initiate at the outersurfaces.3.1.3 biaxial strain amplitude ratioin an axial-torsi
15、onalfatigue test, the biaxial strain amplitude ratio, l is defined as1This practice is under the jurisdiction of ASTM Committee E08 on Fatigue andFracture and is the direct responsibility of Subcommittee E08.05 on CyclicDeformation and Fatigue Crack Formation.Current edition approved May 10, 2002. P
16、ublished August 2002.2Annual Book of ASTM Standards, Vol 03.01.3Annual Book of ASTM Standards, Vol 03.03.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.the ratio of the shear strain amplitude (ga) to the axial strainamplitude (ea),
17、that is, ga/ea.3.1.4 phasing between axial and shear strainsin an axial-torsional fatigue test, phasing is defined as the phase angle, f,between the axial strain waveform and the shear strain wave-form. The two waveforms must be of the same type, forexample, both must either be triangular or both mu
18、st besinusoidal.3.1.4.1 in-phase axial-torsional fatigue testforcompletely-reversed axial and shear strain waveforms, if themaximum value of the axial strain waveform occurs at thesame time as that of the shear strain waveform, then the phaseangle, f = 0 and the test is defined as an “in-phase”axial
19、-torsional fatigue test (Fig. 2(a). At every instant in time,the shear strain is proportional to the axial strain.NOTE 3Proportional loading is the commonly used terminology inplasticity literature for the in-phase axial-torsional loading described inthis practice.3.1.4.2 out-of-phase axial-torsiona
20、l fatigue testforcompletely-reversed axial and shear strain waveforms, if themaximum value of the axial strain waveform leads or lags theFIG. 1 Twisted Gage Section of a Cylindrical Specimen Due to a Torsional MomentFIG. 2 Schematics of Axial and Shear Strain Waveforms for In- and Out-of-Phase Axial
21、-Torsional TestsE 22072maximum value of the shear strain waveform by a phase anglef 0 then the test is defined as an “out-of-phase” axial-torsional fatigue test. Unlike in the in-phase loading, the shearstrain is not proportional to the axial strain at every instant intime. An example of out-of-phas
22、e axial-torsional fatigue testwith f = 75 is shown in Fig. 2(b). Typically, for anout-of-phase axial-torsional fatigue test, the range of f ( 0)is from -90 (axial waveform lagging the shear waveform) to +90 (axial waveform leading the shear waveform).NOTE 4In plasticity literature, nonproportional l
23、oading is the genericterminology for the out-of-phase loading described in this practice.3.1.5 shear stressrefers to engineering shear stress, t,acting in the orthogonal tangential and axial directions of thegage section and is a result of the applied torsional moment, T,to the thin-walled tubular s
24、pecimen. The shear stress, like theshear strain, is always the largest at the outer diameter. Underelastic loading conditions, shear stress also varies linearlythrough the thin wall of the tubular specimen. However, underelasto-plastic loading conditions, shear stress tends to vary in anonlinear fas
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