REG NACA-TN-868-1942 The influence of impact velocity on the tensile characteristics of some aircraft metals and alloys.pdf
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1、sU4mmmi=WJqututu-lmn-i “-1 .k.+4-T-TECHNICALNOTESf-+,f“.-,%blgre”aterthanthe:Increaseof elong,atlon.,Underh.e-”.conditionsof thbsetests, copp$rdoes notseem “tobevbloci,ty-sensiti.ve.“.,.,. .“. .,., :.b.,E.r.ass. T.h.echfige“of“ten-iie,prgpe”rties ofbrsswith velocityseemsto“followthesametendancyfound
2、“withcopper;however,.+hein,cr.e.qs.eof.one”rgyab-sorbedbythealloy is grea”terthag the-increaseshownbpurercopper; . .“ characteristicsseem to var In ahQutQo”e,wayas withptirt3co#per;that i6,:,$ncresoof.ltiWa-ep$rength, ro-ductlonof area,elongationand Anergy”with”iricroasing ve-locity. At first,the in
3、fluenceof velocitySeemsto %esomowhatgl?etiterip the silicon-bron?pthan in pure copper,althoughthis.tendencyis roducedathighervo:locitios.-.,.3.”Steels. “ “” “,. a. SAE 1112 free-cuttingstool.cold-draw% Theyield stresso:fthis mtq.rialincreaq8s,from90,000to130;000ptiundsper squareinchwith rise In rate
4、 of deforma-tion from staticto 20 feet.per,secorid.The,energyrtiqulredto rupturerises from 26.to45 foot-poundsin the same”range.In this.materialthe yie,ldstresswas alw6,yehigherthan theultimatestrengthexcepti.fithe statjictest. d,.b. SAE 1020.hot-ro,lL,ed“steej.-The most effectiveinflu6nce”ofvelocit
5、yon the propertieso.fthis steeZoc- icurs ia the ultimatestrengthwhich ih.qeasesfromabbut65,000to about80,000poundsper sqtireinch.”The reduc-tion of Arearemainsapproxiate.ly:constantthroughoutthevoloci%yrangewhilethe+pe”rce”rik:olonga,tdnis decreasedslightly. Here, again,is a relativelyductilemntoria
6、l xsProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-b+ I?AOATechnicalMote No, 868 15.,.9and ft istebe noted that the yieldy6int in te low-P610Cityrangeincreasesvery markedy- .“ “. . .,.c. SAE 1035 steelfully annealed.-hissteelshowsa markedincrease”of
7、 yield stressfrom 4iiOOOto92,000poundsper squareinch. The ultimate strerigthin-creasesfrom 75,000to 100,000poundsper squareinch. .-The energyrisesfrom”49to 62 foot-pounds. These.in-creasesoccurwithina changein rate of deformationfromstaticto 20 feetper second. At higlter”rates“ofdefor-mation,theyiel
8、d stressrises to 125,000poundsper square inchat 140 feetpe”rsecond,while the ultimatestrengthrisesto a maximumof 115,000pounds-persquareinch at 90feetper secondand then .Unscertain.conditiong,mtixirnuns-”in”the2,400!5,300n,400!7,900NACA TechnicalNote No. 858TABLE IV - ALUMINUMUltimate(lb/sqin.)20,00
9、020,00021,50020,50022,40020,70023,40022,goo2g,20026,50023,20020,60022,goo23,gO022,10020,00025,60020,700Brealklh/sqin.)10,ooo7,0001,()()(110,30011,2009,70010,50011,400n,50015,100lg,ooo15,40017,00016,00015,20013,30014,00011,600015.- 1515.154545%/30* gogo120v 1201201501501504,%;:%57,Om67,500TReduc-Ener
10、gy tionofarea(ftTlb)$7.175.g610.210.4g.g11.p-l11.711.010.311.39.613.111.9I.I -ml!n.gg3,2131m5g204g2.g6.4L .239.246.74-J.:L62g.g30.42G.523 ,Y m12 DN11 DN10 DNzlDNlDN13 m17 m16 DN1311121617 .181920a2223242625 *IN”27 m2g DN29 DN“P Averageness - 59R*DN= doubleneck.Provided by IHSNot for ResaleNo reprodu
11、ction or networking permitted without license from IHS-,-,-. NAGA TechnicalNote Ho. 868 24 J-24S-T ALUMINUMALLOYVelocity Yield Ultinate Break,(ftfsec)(lhfsqtn.) (lb/sqin.) (lbfsqin.)IStatic 46,000 65,600 64,00010 56,000 73s000 63,00037 67,100 77, 65,40064 75,000 a,?300 70,000gg 71,300 76,200 63,o117
12、 79,600 78,000 61,wlW g4,goo 7g,ow 61,500LEnergy(ft-lb)32.046.040.446.946.6Reduc-tionofaea$33.032,740.636a4).041.541.0Elon-gation$.“20.020.222.3 “23.522.02La25.0Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-N.ACATechnialNote No. 868TABLEVII - DOWME
13、TAIIJ, MAGNESIUMALLOY253qleduc-tionofareaI$27.g379537*539.13%436.939.140.139.139.19.1?039:39.1E:ClOnga-tion$5pec-ircenulm-2erCnergy:ft-lb;* velocity Yieldlb/sqin.)30*000jg,gooL9,800,70042,30047,10051,60053,20046,mo58,00062,00069,MO73,20061,70070,30050,000Ultimate(lb/sqin.)Break(lb/sqin.)(ft/see)M2$5
14、67.;10 *DH11 D.N12 DNI-3 DN15 DN16 DN17 DN44,500y,Efoo9,E$ooio,70040,100Zg,goo43,00046,!300i9,500Ji:x9,ooi1,000$2,300lQooW,loo41,00032,10029,30032,50030,60030,600y3,20036,9002g,70032,goo32,20029,goo33,40029,60037,20033370016.715.516.917.41s.217.314.7Ig.116.324.6m.1lg.1s,9lge520.620.315.716.316.716.!
15、317.417.019*319.619.0E1.g20.t322.722.519.122.422*1o101 103030305050z7575100100120120.* Averagehardness-55RTABLEVIII-noln.muX,:3L4GMSIUMALIOYT29.k 14*27.7 14.229.5 1.12g*7 z1 .515.3%: 16.239.1 17.439.2 19030 z1,5002,300U2,6005,000g,40051,60046,700kl,oo46,10042,700z ,000,5009IL212.9-19.3M.g23.4-20.119
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