WA.1816061-T6aluminumalloysheet,stress-straincurvesatroomandelevatedtemperaturesTestedatlowtemperature.Testdirection:longitudinal(top);transverse(bottom).Sheetthickness:2.54mm(0.100in.).Composition:Al-1Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061F.R.Schwartzbergetal,CryogenicMaterialsDataHandbook,ML-TDR-64-280,Aug1964,Suppl.1,Feb1965.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p9WA.1826061-T651aluminumalloyplate,effectofcryogenictemperaturesontensilepropertiesTestedto-269℃(-452°F).Platethickness:31.75mm(1%in.).Composition:Al-1Mg-0.65Si-0.25Cu-0.20Cr.UNSA96061Source:J.G.Kaufman,K.O.Bogardus,andE.T.Wanderer,TensilePropertiesandNotchToughnessofAluminumAlloysat-452FinLiquidHe,Adv.CryogenicEng.,Vol13,1968,p294.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p9WA.1836061-Oaluminumalloy,effectofexposureandtesttemperatureontensilepropertiesExposureupto10,000h.Composition:Al-1Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061Source:“MechanicalPropertiesatVariousTemperaturesof6061-0,”Datasheet,AlcoaResearchLaboratories,1Feb1956.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p9WA.1846061-T4aluminumalloysheet,effectofexposureandtesttemperatureontensilepropertiesComposition:Al-1Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061Source:“MechanicalPropertiesatVariousTemperaturesof6061-T4and6062-T4,”Datasheet,AlcoaResearchLaboratories,23Feb1956.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p10WA.1856061-T6aluminumalloy,effectofexposureandtesttemperatureontensilepropertiesComposition:Al-1Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061Source:"MechanicalPropertiesatVariousTemperaturesof6061-T6Products,”Datatable,AlcoaResearchLaboratories,6Dec1960.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p10Temperature,FWA.1866061-T6aluminumalloysheet,effectoftesttemperatureonstresstoproducevariousamountsofsmallplasticstrainintensionSheetthickness:3.17mm(1/8in.).RT,roomtemperature.Composition:Al-1Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061Source:R.E.MaringerandM.M.Cho,"StabilityofStructuralMaterialsforSpaceCraftApplication,"NASACR97844,NationalAeronauticsandSpaceAdministration,April1968.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p10WA.1876061-T6aluminumalloycladsheet,compressivestress-straincurvesTestedat93,204,and316℃(200,400,and600F)inlongtransversedirection.Composition:Al-1Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061Struc(Source)t:u(M)r(e)e(t)s(a)l,lM(ic)ILM-H(a)tDBK(erials)-5B(an),F(d)SC(E)l15(em)e00(nts),Sept(for)19(A)71(er)opsp(ace)ublish(Vehi)e(cl)d(e)inAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p10WA.1886061-T6aluminumalloysheet,compressivestress-straincurvesTestedat149and260℃(300and500F)inlongtransversedirection.Composition:Al-1Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061Source:MetallicMaterialsandElementsforAerospaceVehicleStructures,MIL-HDBK-5B,FSC1500,Sept1971.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p11WA.1896061-T6aluminumalloysheet,effectoflowtemperatureonshearstrengthTestdirection:Longitudinalandtransverse.Sheetthick-ness:2.54mm(0.100in.).Composition:Al-1.0Mg-0.6Si-0.25Cu-0.20Cr.UNSA96061F.RSchwartzbergetal,CryogenicMaterialsDataHandbook,MIL-TDR-64-280,Aug1964,andSuppl.No.1,Feb1965.AspublishedinAerospaceStructuralMetalsHandbook,Vol3,Code3206,CINDAS/PurdueUniversity,1995,p11WA.1906061-0aluminumalloyrod,tensilestress-straincurvesTheupperrowofstrainvaluesontheabscissaappliestoboththecompletetruecurveandthecompletenominalcurve.Thelowerrowofstrainvaluesappliestotheexpandedportionofthecurves;thisexpandedportionisessentiallyidenticalforboththetrueandnominalcurves.YS,yieldstrength.Testspecimendiam,12.7mm(1/2in.).Gagelength:203.2mm(8in.).Nominaltensilestrength,123MPa(17.8ksi).Truetensilestrength,143MPa(20.7ksi).Nominalyieldstrength(0.2%offset),43MPa(6.2ksi).Elongation(in50.8mm,or2in.),23.4%.Reductionofarea,75%.Truestrainatmaximumload,18.2%.Alog-logplotofthestress-straincurvewouldyieldaslopeof(n)of0.22intheareaofuniformplasticdeformation.UNSA96061Source:Alcoa,AluminumResearchLaboratory,NewKensington,PA,July1954Strain,0.001in./in.WA.1916061-T4aluminumalloyrod,tensilestress-straincurvesTheupperrowofstrainvaluesontheabscissaappliestoboththecompletetruecurveandthecompletenominalcurve.Thelowerrowofstrainvaluesappliestotheexpandedportionofthecurves;thisexpandedportionisessentiallyidenticalforboththetrueandnominalcurves.YS,yieldstrength.Testspecimendiam,12.7mm(1/2in.).Gagelength:203.2mm(8in.).Nominaltensilestrength,285MPa(41.4ksi).Truetensilestrength,307MPa(44:5ksi).Nominalyieldstrength(0.2%offset),190MPa(27.6ksi).Elongation(in50.8mm,or2in.),17.2%.Reductionofarea,54%.Truestrainatmaximumload,7.7%.Alog-logplotofthestress-straincurvewouldyieldaslopeof(n)of0.11intheareaofuniformplasticdeformation.UNSA96061Source:Alcoa,AluminumResearchLaboratory,NewKensington,PA,July1954WA.1926061-T6aluminumalloyrod,tensilestress-straincurvesTheupperrowofstrainvaluesontheabscissaappliestoboththecompletetruecurveandthecompletenominalcurve.Thelowerrowofstrainvaluesappliestotheexpandedportionofthecurves;thisexpandedportionisessentiallyidenticalforboththetrueandnominalcurves.YS,yieldstrength.Testspecimendiam,12.7mm(1/2in.).Gagelength:203.2mm(8in.).Nominaltensilestrength,307MPa(44.5ksi).Truetensilestrength,334MPa(48.5ksi).Nominalyieldstrength(0.2%offset),266MPa(38.6ksi).Elongation(in50.8mm,or2in.),10.8%.Reductionofarea,49%.Truestrainatmaximumload,8.6%.Alog-logplotofthestress-straincurvewouldyieldaslopeof(n)of0.13intheareaofuniformplasticdeformation.UNSA96061Source:Alcoa,AluminumResearchLaboratory,NewKensington,PA,July1954WA.1936061-T6aluminumalloy,allproducts,effectofexposureatelevatedtemperatureonroomtemperaturetensileultimatestrengthExposureupto10,000h,asindicated.Allproducts.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-264WA.1946061-T6aluminumalloysheet,tensilestress-straincurvesTestedatroomtemperature.Typicalforsheetthickness≤6.325mm(≤0.249in.).Ramberg-Osgoodparameter,n(longitudinal,tension)=50;n(longtransverse,tension)=21.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-267WA.1956061-T6aluminumalloysheet,tensilestress-straincurvesTestedat260℃(500°F).Testdirection:longitudinal.Typicalforsheetthickness≤3.175mm(≤0.125in.).Ramberg-Osgoodparameter,n(2-5hexposure)=13;n(10hexposure)=13);n(100hexposure)=13.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-269WA.1966061-T6aluminumalloysheet,compressivestress-strainandcompressivetangentmoduluscurvesTestedatroomtemperature.Testdirection:L,longitudi-nal;LT,longtransverse.Typicalforsheetthickness≤6.325mm(≤0.249in.).Ramberg-Osgoodparameter,n(L,compression)=19;n(LT,compression)=21.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-269WA.1976061-T6aluminumalloysheet,tensileandcompressivestress-strainandcompressivetangentmoduluscurvesTestedatroomtemperature.Testdirection:L,longitudi-nal.Typical.Ramberg-Osgoodparameter,n(L,tension)=50;n(L,compression)=18.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-270WA.1986061-T6aluminumalloyextrusion,tensilestress-straincurvesTestedatroomtemperature.Typicalforallthicknesses.Ramberg-Osgoodparameter,n(longitudinal,tension)=34;n(longtransverse,tension)=29.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-271WA.1996061-T6aluminumalloyextrusion,compressivestress-strainandcompressivetangentmoduluscurvesTestedatroomtemperature.Typicalforallthicknesses.Ramberg-Osgoodparameter,n(longitudinal,compres-sion)=38;n(longtransverse,compression)=28.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-271WA.2006061-T6aluminumalloysheet,tensilestress-straincurve(fullrange)Testedatroomtemperature.Testdirection:longitudinal.Typical.UNSA96061Source:MIL-HDBK-5H,1Dec1998.p3-273WA.2016061-T62aluminumalloyextrusion,tensilestress-straincurves(fullrange)Testedatroomtemperature.Typicalforallthicknesses.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-274WA.2026061-T651X,aluminumalloyextrusion,tensileandcompressivestress-strainandcompressivetangentmoduluscurvesTestedatroomtemperature.Testdirection:L,longitudi-nal;LT,longtransverse.Typicalforextrusionthickness≤12.67mm(≤0.499in.).Ramberg-Osgoodparameter,n(L,tension)=40;n(LT,tension)=19;n(L,compres-sion)=15;n(LT,compression)=14.UNSA96061Source:MIL-HDBK-5H,1Dec1998WA.2036061-T651Xaluminumalloyextrusion,tensileandcompressivestress-strainandcompressivetangentmoduluscurvesTestedatroomtemperature.Testdirection:L,longitudi-nal;LT,longtransverse.Typicalforextrusionthickness≥76.20mm(≥3.000in.).Ramberg-Osgoodparameter,n(L,tension)=45;n(LT,tension)=24;n(L,compres-sion)=40;n(LT,compression)=32.UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-272WA.2046061-T651Xaluminumalloyextrusion,tensilestress-straincurves(fullrange)Testedatroomtemperature.Typicalforextrusionthick-ness≤12.675mm(≤0.499in.).UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-275WA.2056061-T651Xaluminumalloyextrusion,tensilestress-straincurves(fullrange)Testedatroomtemperature.Typicalforextrusionthick-ness76.20mm(3.000in.).UNSA96061Source:MIL-HDBK-5H,1Dec1998,p3-276更多内容见附件免责声明：本页面/内容部分素材来源于互联网公开信息，旨在传递更多信息，不代表本平台立场。版权归原作者或机构所有，如涉及侵权，请通过平台联系我们，我们将在核实后第一时间处理。本平台对转载内容的真实性、准确性不作任何保证，用户需自行判断并承担使用风险。
