ASTM C747-2016 Standard Test Method for Moduli of Elasticity and Fundamental Frequencies of Carbon and Graphite Materials by Sonic Resonance《用声波共振法测定碳和石墨材料弹性模量和基本频率的标准试验方法》.pdf

《ASTM C747-2016 Standard Test Method for Moduli of Elasticity and Fundamental Frequencies of Carbon and Graphite Materials by Sonic Resonance《用声波共振法测定碳和石墨材料弹性模量和基本频率的标准试验方法》.pdf》由会员分享，可在线阅读，更多相关《ASTM C747-2016 Standard Test Method for Moduli of Elasticity and Fundamental Frequencies of Carbon and Graphite Materials by Sonic Resonance《用声波共振法测定碳和石墨材料弹性模量和基本频率的标准试验方法》.pdf（16页珍藏版）》请在麦多课文档分享上搜索。

1、Designation: C747 16 An American National StandardStandard Test Method forModuli of Elasticity and Fundamental Frequencies ofCarbon and Graphite Materials by Sonic Resonance1This standard is issued under the fixed designation C747; the number immediately following the designation indicates the year

2、oforiginal adoption or, in the case of revision, 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. Scope*1.1 This test method covers determination of the dynamicelas

3、tic properties of isotropic and near isotropic carbon andgraphite materials at ambient temperatures. Specimens of thesematerials possess specific mechanical resonant frequencies thatare determined by the elastic modulus, mass, and geometry ofthe test specimen. The dynamic elastic properties of a mat

4、erialcan therefore be computed if the geometry, mass, and mechani-cal resonant frequencies of a suitable (rectangular or cylindri-cal) test specimen of that material can be measured. DynamicYoungs modulus is determined using the resonant frequencyin the flexural or longitudinal mode of vibration. Th

5、e dynamicshear modulus, or modulus of rigidity, is found using torsionalresonant vibrations. Dynamic Youngs modulus and dynamicshear modulus are used to compute Poissons ratio.1.2 This test method determines elastic properties by mea-suring the fundamental resonant frequency of test specimens ofsuit

6、able geometry by exciting them mechanically by a singularelastic strike with an impulse tool. Specimen supports, impulselocations, and signal pick-up points are selected to induce andmeasure specific modes of the transient vibrations. A trans-ducer (for example, contact accelerometer or non-contacti

7、ngmicrophone) senses the resulting mechanical vibrations of thespecimen and transforms them into electric signals. (See Fig.1.) The transient signals are analyzed, and the fundamentalresonant frequency is isolated and measured by the signalanalyzer, which provides a numerical reading that is (or isp

8、roportional to) either the frequency or the period of thespecimen vibration. The appropriate fundamental resonantfrequencies, dimensions, and mass of the specimen are used tocalculate dynamic Youngs modulus, dynamic shear modulus,and Poissons ratio. AnnexA1 contains an alternative approachusing cont

9、inuous excitation.1.3 The values stated in SI units are to be regarded asstandard. No other units of measurement are included in thisstandard.1.4 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

10、 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:2C215 Test Method for Fundamental Transverse,Longitudinal, and Torsional Resonant Frequencies ofConcrete SpecimensC559 Test Method

11、for Bulk Density by Physical Measure-ments of Manufactured Carbon and Graphite ArticlesC885 Test Method for Youngs Modulus of RefractoryShapes by Sonic ResonanceC1161 Test Method for Flexural Strength of AdvancedCeramics at Ambient TemperatureE111 Test Method for Youngs Modulus, Tangent Modulus,and

12、Chord ModulusE177 Practice for Use of the Terms Precision and Bias inASTM Test MethodsE228 Test Method for Linear Thermal Expansion of SolidMaterials With a Push-Rod DilatometerE691 Practice for Conducting an Interlaboratory Study toDetermine the Precision of a Test Method3. Terminology3.1 Definitio

13、ns:3.1.1 antinodes, ntwo or more locations that have localmaximum displacements, called antinodes, in an unconstrainedslender rod or bar in resonance. For the fundamental flexureresonance, the antinodes are located at the two ends and thecenter of the specimen.3.1.2 elastic modulusthe ratio of stres

14、s to strain, in thestress range where Hookes law is valid.3.1.3 flexural vibrations, nthe vibrations that occur whenthe displacements in a slender rod or bar are in a plane normalto the length dimension.1This test method is under the jurisdiction of ASTM Committee D02 onPetroleum Products, Liquid Fu

15、els, and Lubricants and is the direct responsibility ofSubcommittee D02.F0 on Manufactured Carbon and Graphite Products.Current edition approved Oct. 1, 2016. Published January 2017. Originallyapproved in 1974. Last previous edition approved in 2010 as C747 93 (2010)1.DOI: 10.1520/C0747-16.2For refe

16、renced 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.*A Summary of Changes section appears at the end of this standardCopyr

17、ight 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 standardization established in the Decision on Principles for theDevelopment of Internatio

18、nal Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.13.1.4 homogeneous, adjin carbon and graphitetechnology, the condition of a specimen such that the compo-sition and density are uniform, so that any smaller specimentaken from

19、 the original is representative of the whole.Practically, as long as the geometrical dimensions of the testspecimen are large with respect to the size of individual grains,crystals, components, pores, or microcracks, the body can beconsidered homogeneous.3.1.5 in-plane flexure, nfor rectangular para

20、llelepipedgeometries, a flexure mode in which the direction of displace-ment is in the major plane of the test specimen.3.1.6 isotropic, adjin carbon and graphite technology,having an isotropy ration of 0.9 to 1.1 for a specific property ofinterest.3.1.7 longitudinal vibrationswhen the oscillations

21、in aslender rod or bar are in a plane parallel to the lengthdimension, the vibrations are said to be in the longitudinalmode.3.1.8 nodes, none or more locations in a slender rod or barin resonance having a constant zero displacement. For thefundamental flexural resonance of such a rod or bar, the no

22、desare located at 0.224 L from each end, where L is the length ofthe specimen.3.1.9 out-of-plane flexure, nfor rectangular parallelepipedgeometries, a flexure mode in which the direction of displace-ment is perpendicular to the major plane of the test specimen.3.1.10 Poissons ration (), nthe absolut

23、e value of theratio of transverse strain to the corresponding axial strainresulting from uniformly distributed axial stress below theproportional limit of the material. Youngs Modulus (E), shearmodulus (G), and Poissons ratio () are related by thefollowing equation: 5 E 2G! 2 1 (1)3.1.11 resonant fr

24、equency, nnaturally occurring frequen-cies of a body driven into flexural, torsional, or longitudinalvibration that are determined by the elastic modulus, mass, anddimensions of the body. The lowest resonant frequency in agiven vibrational mode is the fundamental resonant frequencyof that mode.3.1.1

25、2 shear modulus, nthe elastic modulus in shear ortorsion. Also called modulus of rigidity or torsional modulus.3.1.13 torsional vibrations, nthe vibrations that occurwhen the oscillations in each cross-sectional plane of a slenderrod or bar are such that the plane twists around the lengthdimension a

26、xis.3.1.14 transverse vibrations, nwhen the oscillations in aslender rod or bar are in a horizontal plane normal to the lengthdimension, the vibrations are said to be in the transverse mode.This mode is also commonly referred to as the flexural modewhen the oscillations are in a vertical plane.3.1.1

27、5 Youngs modulus, nthe elastic modulus in tensionor compression.4. Summary of Test Method4.1 This test method measures the fundamental resonantfrequency of test specimens of suitable geometry (bar or rod)by exciting them mechanically by a singular elastic strike withan impulse tool. A transducer (fo

28、r example, contact accelerom-eter or non-contacting microphone) senses the resulting me-chanical vibrations of the specimen and transforms them intoelectric signals. Specimen supports, impulse locations, andsignal pick-up points are selected to induce and measurespecific modes of the transient vibra

29、tions. The signals areanalyzed, and the fundamental resonant frequency is isolatedand measured by the signal analyzer, which provides a numeri-cal reading that is (or is proportional to) either the frequency orthe period of the specimen vibration. The appropriate funda-mental resonant frequencies, d

30、imensions, and mass of thespecimen are used to calculate dynamic Youngs modulus,dynamic shear modulus, and Poissons ratio.5. Significance and Use5.1 This test method may be used for material development,characterization, design data generation, and quality controlpurposes.5.2 This test method is pri

31、marily concerned with the roomtemperature determination of the dynamic moduli of elasticityand rigidity of slender rods or bars composed of homoge-neously distributed carbon or graphite particles.5.3 This test method can be adapted for other materials thatare elastic in their initial stress-strain b

32、ehavior, as defined inTest Method E111.5.4 This basic test method can be modified to determineelastic moduli behavior at temperatures from 75 C to +2500C. Thin graphite rods may be used to project the specimenextremities into ambient temperature conditions to provideresonant frequency detection by t

33、he use of transducers asdescribed in 7.1.FIG. 1 Block Diagram of Typical Test ApparatusC747 1626. Interferences6.1 The relationships between resonant frequency and dy-namic modulus presented herein are specifically applicable tohomogeneous, elastic, isotropic materials.6.1.1 This method of determini

34、ng the moduli is applicableto inhomogeneous materials only with careful consideration ofthe effect of inhomogeneities and anisotropy. The character(volume fraction, size, morphology, distribution, orientation,elastic properties, and interfacial bonding) of inhomogeneitiesin the specimens will have a

35、 direct effect on the elasticproperties of the specimen as a whole. These effects must beconsidered in interpreting the test results for composites andinhomogeneous materials.6.1.2 The procedure involves measuring transient elasticvibrations. Materials with very high damping capacity may bedifficult

36、 to measure with this technique if the vibration dampsout before the frequency counter can measure the signal(commonly within three to five cycles).6.1.3 If specific surface treatments (coatings, machining,grinding, etching, etc.) change the elastic properties of thenear-surface material, there may

37、be accentuated effects on theproperties measured by this flexural method, as compared tostatic bulk measurements by tensile or compression testing.6.1.4 The test method is not satisfactory for specimens thathave major discontinuities, such as large cracks (internal orsurface) or voids.6.2 This test

38、method for determining moduli is limited tospecimens with regular geometries (rectangular parallelepipedand cylinders) for which analytical equations are available torelate geometry, mass, and modulus to the resonant vibrationfrequencies. The test method is not appropriate for determiningthe elastic

39、 properties of materials that cannot be fabricated intosuch geometries.6.2.1 The analytical equations assume parallel and concen-tric dimensions for the regular geometries of the specimen.Deviations from the specified tolerances for the dimensions ofthe specimens will change the resonant frequencies

40、 and intro-duce error into the calculations.6.2.2 Edge treatments such as chamfers or radii are notconsidered in the analytical equations. Edge chamfers onflexure bars prepared according to Test Method C1161 willchange the resonant frequency of the test bars and introduceerror into the calculations

41、of the dynamic modulus. It isrecommended that specimens for this test method not havechamfered or rounded edges.6.2.3 For specimens with as-fabricated and rough or unevensurfaces, variations in dimensions can have a significant effectin the calculations. For example, in the calculation of dynamicmod

42、ulus, the modulus value is inversely proportional to thecube of the thickness. Uniform specimen dimensions andprecise measurements are essential for accurate results.6.3 The test method assumes that the specimen is vibratingfreely, with no significant restraint or impediment. Specimensupports should

43、 be designed and located properly in accor-dance with 9.3.1, 9.4.1, and 9.5.1 so the specimen can vibratefreely in the desired mode. In using direct contact transducers,the transducer should be positioned away from antinodes andwith minimal force to avoid interference with free vibration.With non-co

44、ntacting transducers, the maximum sensitivity isaccomplished by placing the transducer at an antinode.6.4 Proper location of the impulse point and transducer isimportant in introducing and measuring the desired vibrationmode. The locations of the impulse point and transducer shouldnot be changed in

45、multiple readings; changes in position maydevelop and detect alternative vibration modes. In the samemanner, the force used in impacting should be consistent inmultiple readings.6.5 If the frequency readings are not repeatable for aspecific set of impulse and transducer locations on a specimen,it ma

46、y be because several different modes of vibration arebeing developed and detected in the test. The geometry of thetest bar and desired vibration mode should be evaluated andused to identify the nodes and antinodes of the desiredvibrations. More consistent measurements may be obtained ifthe impulse p

47、oint and transducer locations are shifted to induceand measure the single desired mode of vibration.7. Apparatus7.1 Apparatus suitable for accurately detecting, analyzing,and measuring the fundamental resonant frequency or period ofa vibrating free beam is used. The test apparatus is shown inFig. 1.

48、 It consists of an impulser, a suitable pickup transducerto convert the mechanical vibration into an electrical signal, anelectronic system (consisting of a signal conditioner/amplifier,a signal analyzer, and a frequency readout device), and asupport system. Commercial instrumentation is available t

49、hatmeasures the frequency or period of the vibrating specimen.7.2 ImpulserThe exciting impulse is imparted by lightlystriking the specimen with a suitable implement. This imple-ment should have most of its mass concentrated at the point ofimpact and have mass sufficient to induce a measurablemechanical vibration, but not so large as to displace or damagethe specimen physically. In practice, the size and geometry ofthe impulser depends on the size and weightand elasticproperties of the specimen and the force needed to producevibration. For comm