REG NACA-TN-3462-1955 Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load.pdf
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1、c_(D-T6.- Master yield and rupture curves for7075-T6 employing the linear temperature parameter (2) are shown in fig-ure 23. Good correlation was found particularly for yield temperaturesat 40 ksi and 60 ksi where the test points are closely superimposed. Thecorrelation for rupture temperatures is f
2、airly good except at 40 ksi wherethe scatter of the data is considerable.The master curves for yield and rupture are linear from about 17 ksito 65 ksi. The yield stress _y, which corresponds to the yield tempera-ture Ty, may be expressed asI Ty + 2O071Oy = 133.5 - 2.55iog h + iThe rupture stressbe g
3、iven asor at which the rupture temperature_Tr + 2007)Or = 143.5 - 2-69_iog h +Tr occurs may(6)Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACA TN3462 iiIn equations (5) and (6), the stresses Sy and _r are in ksi, thetemperatures Ty and Tr are in
4、OF, and the temperature rate h is inOF per second. These formulas are limited to stresses from 17 ksi to65 ksi.The correlation of the data for yield and rupture temperaturesemploying the reciprocal temperature parameter (4) was almost identicalwith that obtained with the linear parameter (2). Conseq
5、uently, themaster curves based on the reciprocal parameter are not included.The validity of the linear parameter is shown by the correlation ofthe data with the master curves (fig. 23). A more critical evaluationof the accuracy obtainable by the use of the master curve and the param-eter may be had
6、by making a comparison of predicted or calculated yieldand rupture temperatures with the test results at different stress levels.Calculated yield temperatures (fig. 12) agree within 10o F with the testresults. Calculated rupture temperatures (fig. 16) are also in closeagreement with the test results
7、 except at 40 ksi where there is a maximumdifference of about 20 F. Similar calculations, based upon the mastercurves, using the reciprocal temperature parameter (4) were in very closeagreement with those shown in figures 12 and 16.Master curves for 2024-T3.- Master yield and rupture curves for2024-
8、T3 usingthe linear temperature parameter (5) are shown in figure 24.The correlation of the data is not so good for this material as thatobtained for 7075-T6 (fig. 23). The correlation is very poor at 50 ksifor yield temperatures and only fair at 40 ksl for rupture temperatures.The master curves for
9、yield and rupture can be assumed to be linearover part of the range. The yield stress ay under rapid-heating con-ditions can be given asThe rupture stressrY + 20091_y = 106.0 - 2.03 og h + 1_r can be expressed as(7)(8)Tr+ 20091_r = 127.5 - 2.38iog h + iIn equations (7) and (8), the stresses _y and _
10、r are in ksi, thetemperatures Ty and Tr are in OF, and the temperature rate h isProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-12 NACATN3462in OF per second. Equations (7) and (8) are limited, respectively, tothe 16-ksi to 40-ksi and 16-ksi to 50-ks
11、i ranges.As in the case of 7075-T6, the correlation of the data for yieldand rupture employing the reciprocal temperature parameter (4) waspractically the sa_e as that obtained with the linear temperatureparameter (2). Master curves b_sed on the former are therefore notincluded.Calculated yield and
12、rupture temperatures based upon the use ofthe linear temperature parameter are comparedwith the test results infigures 13 and 17. Fair agreement is obtained except at 50 ksi for yieldtemperatures and at 40 ksl for rupture temperatures. The agreementbetween calculated and experimental results_ howeve
13、r_ is not so good forthis material as that for 7075-T6 (figs. 12 and 16). It is not surprisingthat the sameparameters do not work so well for 2024-T3 as for 7075-T6because aging of the former markedly alters the general pattern of theresults. Calculated yield and rupture temperatures_ obtained by me
14、ansof the reciprocal temperature parameter (4), were in close agreementwith those shownfor the linear temperature parameter (3)-CONCLUDINGIn the rapid-heating tensile tests of 7075-T6 and 2024-T3 aluminum-alloy sheet under constant load and temperature rates from 0.2 F toi00 F per second, yield and
15、rupture temperatures were found to increaseapproximately in proportion to the logarithm of the temperature rateexcept in certain regions for 2024-T3 aluminumalloy where aging affectedthe results.Under rapid-heating conditions_ yield and rupture stresses maybesubstantially greater or about the samefo
16、r a given temperature as corre-ponding stresses obtained from elevated-temperature tensile stress-straintests for i/2-hour exposure, depending upon the temperature rate andmaterial. The increase in yield and rupture stresses with temperaturerates for a given temperature becomesfairly small at rates
17、above60 F per second.Linear and reciprocal temperature-rate parameters madeit possibleto take into account the effect of the temperature rate and to constructsingle or master curves of stress against the parameter. These curvesprovide a convenient method of obtaining yield and rupture stresses andPr
18、ovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACATN 5462 15temperatures for a given temperature rate. Good correlation of the datawith the master curves was obtained except where aging altered theresults.Langley Aeronautical Laboratory,National Advi
19、sory Committee for Aeronautics,Langley Field, Va._ March 25, 1955-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-14 NACATN3462APPENDIXDESCRIPTIONOFTESTEQUIPMENTFORRAPID-HEATINGTESTSLoading EquipmentThe general arrangement of the loading equipment is
20、 shown in fig-ure 2. The load was applied to the specimen through a 5:1 beamor leversystem by meansof weights. The fulcrum of the beamwas supported on aplate mounted near the top of the three columns of a 120,O00-pound-capacity two-way hydraulic Jack. The weight-loading system had a maxi-mumcapacity
21、 of lO,000 pounds on the specimen. Knife edges were employedat the fulcrum and other loading points of the beam. With this system,the beamcould be positioned and the weight cage could be lifted fromthe floor by lowering the ram of the two-way Jack.The method of connecting the specimen to the loading
22、 system is shownin more detail in figure 5. The load was applied to the specimenby meansof yoke-and-pin connections. In order to prevent grounding at the top andbottom of the specimen, which was part of the electrical circuit, theloading bars were electrically insulated from the rest of the system.T
23、his insulation was provided by the two-plece rectangular load insulatorsshownabove the top column plate and above the ram.Because a discontinuity of slope was obtained in the tlme-temperaturerecords at the beginning of heating, the possibility of inertia effectsin the load system was investigated. L
24、oad variations were measuredbymeansof a calibration bar in series with the specimen. The variationin output of two wire strain gages mounted on the bar was measuredwitha pen-type recorder with a 100-cycle-per-second response. No detectablevariations in load occurred within the range of temperature r
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