ASTM D2718-2000(2006) Standard Test Methods for Structural Panels in Planar Shear (Rolling Shear)《结构受力壁板平面剪切(滚剪)的试验方法》.pdf

上传人:progressking105 文档编号:513407 上传时间:2018-12-02 格式:PDF 页数:6 大小:144.55KB
下载 相关 举报
ASTM D2718-2000(2006) Standard Test Methods for Structural Panels in Planar Shear (Rolling Shear)《结构受力壁板平面剪切(滚剪)的试验方法》.pdf_第1页
第1页 / 共6页
ASTM D2718-2000(2006) Standard Test Methods for Structural Panels in Planar Shear (Rolling Shear)《结构受力壁板平面剪切(滚剪)的试验方法》.pdf_第2页
第2页 / 共6页
ASTM D2718-2000(2006) Standard Test Methods for Structural Panels in Planar Shear (Rolling Shear)《结构受力壁板平面剪切(滚剪)的试验方法》.pdf_第3页
第3页 / 共6页
ASTM D2718-2000(2006) Standard Test Methods for Structural Panels in Planar Shear (Rolling Shear)《结构受力壁板平面剪切(滚剪)的试验方法》.pdf_第4页
第4页 / 共6页
ASTM D2718-2000(2006) Standard Test Methods for Structural Panels in Planar Shear (Rolling Shear)《结构受力壁板平面剪切(滚剪)的试验方法》.pdf_第5页
第5页 / 共6页
亲,该文档总共6页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、Designation: D 2718 00 (Reapproved 2006)Standard Test Methods forStructural Panels in Planar Shear (Rolling Shear)1This standard is issued under the fixed designation D 2718; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year

2、 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 These test methods determine the shear properties ofstructural panels associated with shear distortion of the pla

3、nesparallel to the edge planes of the panels. Both shear strengthand modulus of rigidity may be determined. Primarily, the testsmeasure the planar shear (rolling shear) strength developed inthe plane of the panel.1.2 Structural panels in use include plywood, waferboard,oriented strand board, and com

4、posites of veneer and ofwood-based layers.1.3 Two test methods are included:1.3.1 Test Method APlanar shear loaded by plates.1.3.2 Test Method BPlanar shear induced by five-pointbending.1.3.3 The choice of method will be dictated by the purposeof the test and equipment available.1.3.4 Test Method A,

5、 Planar Shear Loaded by PlatesThistest method uses a rectangular panel section adhered betweensteel plates with protruding knife edges to create load at thepanel faces. This test method has been used to develop shearproperties of plywood and oriented strand board for thepurpose of confirming design

6、values. This test method does notproduce pure shear, but the specimen length is prescribed sothat the secondary stresses have a minimum effect. The methoddetermines shear strength and modulus of rigidity.1.3.5 Test Method B, Planar Shear Induced by Five-PointBendingPlanar shear stress is induced on

7、the panel whileloaded in bending using two continuous spans. This testmethod determines planar shear strength consistent with panelapplications under transverse loading. This test method is ableto determine shear strength at any moisture condition.1.4 This standard does not purport to address all of

8、 thesafety concerns, if any, associated with 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:2D 2395 Test Methods for

9、Specific Gravity of Wood andWood-Based MaterialsD 4442 Test Methods for Direct Moisture Content Measure-ment of Wood and Wood-Base Materials3. Significance and Use3.1 Planar shear (rolling shear) characteristics of structuralpanels determined by these test methods are essential for therigorous desig

10、n of various glued wood-panel structural com-ponents, such as box beams, folded plate roofs, and stressedskin panels. Planar shear also may govern the design at lowspan-depth ratios encountered in floors subjected to highconcentrated loads, concrete forms at high pouring pressures,and bulk storage s

11、tructures.3.2 The modulus of rigidity determined from Test MethodAis a composite of the entire specimen acting as a unit. Forplywood panels for which the ratio between the shear moduliof the plies with grain oriented parallel and perpendicular to theshear forces is known, the rolling shear modulus o

12、f theperpendicular plies can be calculated.3.3 Veneer produced by slicing or rotary peeling maycontain fine checks or separations parallel to the grain on theknife side of the veneer that are produced as the knife is forcedthrough the wood. These checks are termed “knife checks” todistinguish them f

13、rom occasional checks that may be formedon the opposite side of the veneer by forces at the compressionbar, and from checks caused by drying. Knife checks can havea significant effect on rolling shear properties in plywoodpanels and may be of significance in other veneer containingpanels. Test Metho

14、dArequires (when applicable) the testing of1This test method is under the jurisdiction of ASTM Committee D07 on Woodand is the direct responsibility of Subcommittee D07.03 on Panel Products.Current edition approved Oct. 1, 2006. Published October 2006. Originallyapproved in 1969. Last previous editi

15、on approved in 2000 as D 2718 00e1.2For 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.1Copyright ASTM Internatio

16、nal, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.matching specimens having knife checks oriented both openand closed wherever possible (see Fig. 1).3.4 To control or define other variables influencing rollingshear, these test methods require determination of m

17、oisturecontent, specific gravity, and elapsed time-to-failure. Condi-tioning of test material in controlled atmospheres, determina-tion of depth of knife checks (when applicable), and determi-nation of percent of wood and plywood glueline failure (whenapplicable) are recommended.4. Control of Moistu

18、re Content4.1 The structural panel samples to be tested at specificmoisture contents or equilibrium relative humidities shall beconditioned to approximately constant weight in controlledatmospheric conditions before gluing to plates. For approxi-mating moisture conditions of structural panel used un

19、der dryconditions a relative humidity of 65 6 2 % at a temperature of68 6 6F (20 6 3C) is recommended. Specimens shall betested without undue delay after the adhesive is cured. Testingin similarly controlled atmospheres is recommended whereverpossible.Test Method APlanar Shear Loaded by Plates5. Sco

20、pe5.1 The specimen having the form of a rectangular flat plateis bonded between steel plates beveled at opposite ends of thespecimen to provide knife edges for loading the plate at theface bonded to the specimen. The knife edges project beyondthe ends of the specimen. This test method is conducted b

21、yloading the knife edges in compression at a uniform rate whilea suitable gage measures slip between the plates due tospecimen deformation. Shear strength is computed from maxi-mum load, and effective shear modulus for the specimen isdetermined from a plot of load versus slip.6. Test Specimen6.1 Spe

22、cimen thickness shall be that of the material. Speci-mens from material that is expected to vary significantly withinthe specimen due to growth or manufacturing features or fromother causes shall be 6 in. (15 cm) wide by 18 in. (45 cm) longor larger as shown in Fig. 2. This size is recommended forun

23、iform material as well. However, smaller specimens ofuniform material may be used if these are not less than fourtimes the thickness in width nor twelve times the thickness inlength.6.2 From each sample of panels containing veneer, twomatching specimens shall be cut. Knife edges of loading platesfor

24、 one specimen of each matching pair shall be orientedperpendicular to one of the primary panel directions or forplywood to cause opening of knife checks during test as shownin Fig. 1(a). Knife edges of plates loading the other specimenshall be positioned perpendicular to one of the primary paneldire

25、ctions or for plywood to cause knife checks to close duringtest as shown in Fig. 1(b). Proper plywood orientation may bedetermined from check depth specimens described in 16.3.Itmay not be possible to test samples having two or more pliesstressed in rolling shear in both “open” and “closed” orienta-

26、tions if these plies are oriented in opposite directions causinga“ checks open” failure regardless of direction of loading.6.3 Specimen length and width shall be measured to thenearest 0.01 in. (0.25 mm) and thickness to the nearest 0.001in. (0.025 mm). When applicable, the direction of knife checks

27、in plies having grain perpendicular to its length shall bedetermined and the specimens marked for position of knifeedges. At the time specimens are cut matching samples fordetermination of moisture content and specific gravity inaccordance with 16.1 and 16.2 shall be obtained. Whenmeasurement of kni

28、fe checks is included as discussed in 16.3,a sample for this measurement also may be cut at this time.7. Loading7.1 Figs. 1 and 2 illustrate the specimen and suitable loadingplates and blocks for loading the knife edges of the plates. The(a) Knife Checks Open(b) Knife Checks ClosedFIG. 1 Orientation

29、 of Knife Checks in PlywoodNOTEThe “V” block is supported on a seat that provides rotationabout the axis perpendicular to the knife edge only.Metric Equivalentsin. 6 18mm 15 45FIG. 2 Planar (Rolling) Shear Test Using a Dial Gage forMeasuring Plate SlipD 2718 00 (2006)2specimen shall be loaded by ste

30、el plates bonded to both facesof the specimen with an adhesive sufficiently rigid to precludecontribution of adhesive creep to measured deformation. Widthof plates shall be that of the specimen. One end of each plateshall be provided with a knife edge projecting14 in. (6 mm)beyond the end of the spe

31、cimen at one end and flush with thesurface glued to the specimen. The other end of the plate shallbe square and flush with the end of the specimen. Knife edgesof the two plates shall be at opposite ends of the specimen andshall be oriented to load the specimen in the desired directionin relation to

32、the knife checks. Planar shear properties ofstructural panels should be determined in both directions.Plates for specimens 18 in. (45 cm) long shall be 1 in. (2.5 cm)thick. The thickness of plates for shorter specimens may bereduced proportionately. Loading of at least one V-block shallprovide for u

33、niform load distribution along the knife edge byloading through a pivot having its axis perpendicular to theknife edge and centered along it. Pivots permitting rotationabout an axis parallel to the knife edge or spherical seats freeto pivot in this manner shall not be used as they create unstableloa

34、ding which may cause violent ejection of the specimen fromthe machine and hazard to operating personnel. The V-blocksshall be vertically positioned in the machine, one above theother, causing the forces applied to the specimen to act parallelto the axis of the machine. The specimen itself will be sl

35、ightlyinclined when placed in the machine. A means of holding theplates in an upright position after the specimen has shearedapart is desirable as a complete separation of the specimenpermits the plates to be thrown out of the machine withattendant hazard to the operator.7.2 Load shall be applied co

36、ntinuously throughout the test atconstant rate of cross-head motion to normally produce failurein the range of 3 to 12 min elapsed time from beginning ofloading. For plywood, the approximate speed may be deter-mined as follows:N 5 0.0075 (T|1 R(T! (1)where:N = crosshead speed, in./min (cm/min),(T|=

37、total thickness of plies having grain parallel todirection of shear force, in. (cm),R = 8 (assumed ratio of shear modulus of parallel pliesto shear modulus of perpendicular plies), and(T= total thickness of plies having grain perpendicularto the direction of shear force, in. (cm).7.2.1 Elapsed time

38、from beginning of load application tofailure of each specimen shall be measured and recorded to thenearest half minute. Machine speeds calculated by the aboveformula will normally produce failure in the range of 3 to 12min elapsed time from the beginning of loading. Shouldelapsed time to failure fal

39、l greatly outside this range, machinespeed should be modified to obtain times within this range.7.3 Both epoxy and polyvinyl adhesives have been foundsatisfactory for bonding steel plates to specimens. Minimumrequired surface preparation of steel plates consists of removalof residual adhesive. This

40、can be accomplished most easily bymild heating of the plate and any portion of the specimenremaining from the previous test in an oven which weakens thebond to the steel sufficiently to permit peeling the remainingwood and adhesive from the plate. The residual adhesive maybe scraped off with a sharp

41、-edged tool. Further degreasing andcleaning has frequently been found necessary in addition to theabove to ensure adequate bond strength. Curing the adhesive ata slightly elevated temperature has also been helpful.8. Measurement of Deformation8.1 Slip between the steel plates during load application

42、shall be measured to at least the nearest 0.0001 in. (0.002 mm)at no less than twelve and preferably more equally spacedincrements of load to proportional limit from which a load-deformation curve shall be plotted. Slip can be measured witha dial gage as illustrated in Figs. 2 and 3 or with appropri

43、ateautomatic measuring and recording equipment. Gage geometryand position on the specimen shall be such as to minimize anyeffects of unsymmetrical loading or deformation.9. Calculation9.1 Shear stress shall be calculated as follows:fv5 P/LW! (2)where:fv= shear stress, psi (N/mm),P = maximum or propo

44、rtional limit load (force), lbf (N),W = specimen width, in. (mm), andL = specimen length, in. (mm).Maximum shear stress obtained from specimens having finalfailure of the bond between the plate and the specimen shall beregarded as defective and shall be clearly indicated in thereport of results.9.2

45、Effective modulus of rigidity for the specimen acting asa unit shall be calculated as follows:G 5 P/D!t/LW!# (3)where:G = apparent modulus of rigidity for the entire speci-men, psi (N/mm),t = specimen thickness, in. (mm),P/D = slope of the force-deformation curve below propor-tional limit load, lbf/

46、in. (N/mm), and other notationis as indicated in 9.1.For plywood, modulus of rigidity of the cross plies may becalculated from that given above if the ratio of moduli ofrigidity and thickness of the parallel and perpendicular plies isknown.D 2718 00 (2006)3Test Method BPlanar Shear Induced by Five-P

47、ointBending10. Scope10.1 Specimens are tested in a two-span continuous beamsupport configuration with line loads applied at midspan ofeach span as shown in Fig. 4. Induced shear stresses areconsistent with those developed in conventional panel appli-cations under transverse loading. Specimens may be

48、 tested inany moisture condition.NOTE 1Research that led to the development of the test method isavailable.3,4Research on the test methods usefulness for determiningelastic constants is also available.511. Test Specimen11.1 The test specimen shall be rectangular in cross-section.The depth of the spe

49、cimen shall be the thickness of thematerial, and the width shall be at least 4.5 in. (115 mm) andno greater than 10 in. (255 mm) (see Note 2).NOTE 2Specimen width may be modified for practical purposes.Since shear strength may vary slightly with specimen width, specimenwidth shall be reported with shear strength results.11.2 MeasurementsSpecimen thickness and width shallbe measured to the nearest 0.001 in. (0.02 mm) at midlength(over center support) and at midspan (under line loads).Thickness measurements shall be determined at these locationson each side of

展开阅读全文
相关资源
猜你喜欢
  • ASD-STAN PREN 4273-1997 Aerospace Series Aluminium Alloy AL-P6082-T6511 Extruded Bar and Section a or D Less than or Equal to 200 mm (Edition P 1)《航空航天系列 铝合金AL-P6082-T6511制a或D≤200m.pdf ASD-STAN PREN 4273-1997 Aerospace Series Aluminium Alloy AL-P6082-T6511 Extruded Bar and Section a or D Less than or Equal to 200 mm (Edition P 1)《航空航天系列 铝合金AL-P6082-T6511制a或D≤200m.pdf
  • ASD-STAN PREN 4274-1997 Aerospace Series Aluminium Alloy AL-P6082-T6511 Extruded Bar and Section a or D Less Than or Equal to 200 mm with Peripheral Coarse Grain Control (Edition P.pdf ASD-STAN PREN 4274-1997 Aerospace Series Aluminium Alloy AL-P6082-T6511 Extruded Bar and Section a or D Less Than or Equal to 200 mm with Peripheral Coarse Grain Control (Edition P.pdf
  • ASD-STAN PREN 4275-1997 Aerospace Series Aluminium Alloy AL-P7075-T76511 Extruded Bar and Section a or D Less than or Equal to 100 mm with Peripheral Coarse Grain Control (Edition .pdf ASD-STAN PREN 4275-1997 Aerospace Series Aluminium Alloy AL-P7075-T76511 Extruded Bar and Section a or D Less than or Equal to 100 mm with Peripheral Coarse Grain Control (Edition .pdf
  • ASD-STAN PREN 4276-1998 Aerospace Series Aluminium Alloy AL-P7175-T7351 Hand Forgings a Less Than or Equal to 150mm (Edition P 1)《航空航天系列 a≤150mm的铝合金AL-P7175-T7351手制锻件 第P1版》.pdf ASD-STAN PREN 4276-1998 Aerospace Series Aluminium Alloy AL-P7175-T7351 Hand Forgings a Less Than or Equal to 150mm (Edition P 1)《航空航天系列 a≤150mm的铝合金AL-P7175-T7351手制锻件 第P1版》.pdf
  • ASD-STAN PREN 4277-1998 Aerospace Series Aluminium Alloy AL-P7175-T73 Hand and Die Forgings a Less Than or Equal to 125 mm (Edition P 1)《航空航天系列 a≤125mm的铝合金AL-P7175-T73手制锻件和模锻件 第P1版.pdf ASD-STAN PREN 4277-1998 Aerospace Series Aluminium Alloy AL-P7175-T73 Hand and Die Forgings a Less Than or Equal to 125 mm (Edition P 1)《航空航天系列 a≤125mm的铝合金AL-P7175-T73手制锻件和模锻件 第P1版.pdf
  • ASD-STAN PREN 4278-1998 Aerospace Series Aluminium Alloy AL-P7175-T7352 Hand and Die Forgings a Less Than or Equal to 150 mm (Edition P 1)《航空航天系列 a≤150mm的铝合金AL-P7175-P7352手制锻件和模锻件 .pdf ASD-STAN PREN 4278-1998 Aerospace Series Aluminium Alloy AL-P7175-T7352 Hand and Die Forgings a Less Than or Equal to 150 mm (Edition P 1)《航空航天系列 a≤150mm的铝合金AL-P7175-P7352手制锻件和模锻件 .pdf
  • ASD-STAN PREN 4282-1998 Aerospace Series Aluminium Alloy AL-P2219-T37 Plate 6 mm Less Than a Less Than or Equal to 40 mm (Edition P 1)《航空航天系列 AL-P2219-T37铝合金制6mm<a≤40mm厚板材 第P1版》.pdf ASD-STAN PREN 4282-1998 Aerospace Series Aluminium Alloy AL-P2219-T37 Plate 6 mm Less Than a Less Than or Equal to 40 mm (Edition P 1)《航空航天系列 AL-P2219-T37铝合金制6mm<a≤40mm厚板材 第P1版》.pdf
  • ASD-STAN PREN 4283-2003 Aerospace Series Aluminium Alloy AL-P2219-T87 Plate 6 mm Less Than a Less Than or Equal to 40 mm (Edition P 2)《航空航天系列 AL-P2219-T87铝合金制6mm<a≤40mm厚板材 第P2版》.pdf ASD-STAN PREN 4283-2003 Aerospace Series Aluminium Alloy AL-P2219-T87 Plate 6 mm Less Than a Less Than or Equal to 40 mm (Edition P 2)《航空航天系列 AL-P2219-T87铝合金制6mm<a≤40mm厚板材 第P2版》.pdf
  • ASD-STAN PREN 4284-1998 Aerospace Series Aluminium Alloy AL-P2219-T852 Forgings a Less Than or Equal to 400 mm (Edition P 1)《航空航天系列 铝合金AL-P2219-T852制a≤400mm的锻件 第P1版》.pdf ASD-STAN PREN 4284-1998 Aerospace Series Aluminium Alloy AL-P2219-T852 Forgings a Less Than or Equal to 400 mm (Edition P 1)《航空航天系列 铝合金AL-P2219-T852制a≤400mm的锻件 第P1版》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ASTM

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1