NASA-TN-3604-1956 Low-speed yawed-rolling characteristics and other elastic properties of a pair of 26-inch-diameter 12-ply-rating type VII aircraft tires《一对26 in直径12线网层率的VII类型飞机轮胎.pdf
《NASA-TN-3604-1956 Low-speed yawed-rolling characteristics and other elastic properties of a pair of 26-inch-diameter 12-ply-rating type VII aircraft tires《一对26 in直径12线网层率的VII类型飞机轮胎.pdf》由会员分享,可在线阅读,更多相关《NASA-TN-3604-1956 Low-speed yawed-rolling characteristics and other elastic properties of a pair of 26-inch-diameter 12-ply-rating type VII aircraft tires《一对26 in直径12线网层率的VII类型飞机轮胎.pdf(99页珍藏版)》请在麦多课文档分享上搜索。
1、mmU3. _f“FORAERONAUTICSTECHNICAL NOTE 3604YAWED-ROLLING CHARACTERISTICSANDL_OTHER ELASTICPROPERTIES OF A PAIR OF 26-CH-DIA.METER, 12-PLY-RATG,TYPE Vu AIRCRAFT TIRESBy Walter B. Home, Robert F. Smiley,and Bertrand H. StephensonLangley Aeronautical LaboratoryField, Va.Washingtonmy 1956., . - ,=3,-:_ .
2、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TECHLIBRARYKAFBJNM,NATIONALADVISORYCOMITTEEFORAERONAUTICS lullullllHlll#00bb511aTMXNl_CALNO17JZ3604LOW-SPEEDYAWED-ROLLINGCHARACTERISTICSANDOTHERELASTICPROPERTIESOFA PAIROF26-RWH-DIAMEIER,12-PLY-RATING,T
3、YPEVIIAIRCRAFTTIRESByWalterB.Home,RobertF.Smiley,andBertrandH.StephensonEmMARYThelow-speed(upto2milesperhour)corneringcharacteristicsoftwo26x 6.6,ty-peVII,1.2-ply-ratingtiresunderstraight-yawedrollinnweredeterminedoverarangeofinflationpressuresandyawanglesfortwoverticalloads,oneloadapproximatelyequa
4、ltotheratedverticalloadandtheotherloadapproximatelyequaltotwicetheratedverticalloadforthesetires.Thecorneringchsracterin.GTirecircumference9aperipheraldistancemoundtire,in.time,secrollingvelocity,in/see.maxi.mmtirewidth,in.displacementindirectionofmotion,in.verticaltiredeflectionduetocmibinedh.verti
5、caltire*flectionduetoverticalorftin.verticalandyawloadonly,in.,.,!-loads,.vProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACATN3604 5ener-dissipationparameterforstaticlateral-elasticitytestsreductioninoscillationsmplitudepercycleenergy-dissipationp
6、ersmeterfordynamiclateral-elasticitytests,2(1-qp)(1+ llJlateraldistortionoftireequator,in.lateraldistortionofthe equatoratcenterofcontact,in.maximumdragcoefficientoffriction,Fx,n,?zsliding-dragcoefficientoffriction,Fx,n,s/Fzyawed-rollingcoefficientof.friction,?R,r,e,tizturningradius,fttorsionoryawan
7、gle,degwheelangularvelocity,radians/seeSubscripts:e eqydl.ibriumorsteady-staterollingconditionm msximumn nonrollingconditionr rollgconditions slidingconditionBarsoversymbolsdenotetheaveragevaluesofthequantitiesinvolvedfortiresA andB. .-. ._ ._ _ .-. _ _ .Provided by IHSNot for ResaleNo reproduction
8、or networking permitted without license from IHS-,-,-6AFPARATWTestVehicleNACATN3604Thebasictestvehicleconsistsofthefuselageandwingcentersectionofa cargoairplanewhichwastowedtailfirstbyatractortruckatanattitudesuchthattheoriginalairplaneshockstrutswerenesrlyvertical.Theoriginalyokessadtorquelinksofth
9、elanding-gearstrutsalongwiththewheelassemblieswerereplacedbysteelwheelhousingswhichheldthetiresandwheelstested.Thesesteelwheelhousingswereconnectedtogetherbymeansofaninstrumentedtruss.Holeslocatedinthewheelhousingatregularintervalsof“ permittedthewheelframestoberotatedthroughayaw-anglerangefrom0to24
10、.50toeout. (Itmightbenotedthata smalli.nitialmisaUnementofthewheelsofapproxi-mately0.3,whichwasnotedinref.3,waseliminatedforthepresentinvestigation.)A sketchofthebssictestvehicleisshowninfigure1.AmOredetaileddescriptionofthistestvehicleisgiveninreference3andappliesingeneraltothepresentinvestigation.
11、Theweightofthetestiehicleactingonthetiresforthelight-weightconditiontestedwasapproximately9,000poundsforeachthe. Fortheheavy-weightconditiontested,a concreteweightcan(weighingapproxi-mately8,OOOpounds)wasattachedtoeachwings-bib.(Seefig.2.) Thisweightincreasedtheloadoneachthe toapproximately17,100pmn
12、ds. The “maximumtowingforcerequiredwasapproximately4,000poundsforeachttre.InstrumentationThetestvehiclewasequippedwithinstrumentsformeasuringside force,torsionalnmment(self-aliningtorquefortheyawed-rollingcese),drag,verticaltiredeflection,horizontaltranslation,andwheelrota-tion.Measurementsofthesequ
13、antitieswererecordedsimultaneouslyonalchannelrecordingoscillographmountedinthetestvehicle.ThisoscillographwasequippedwithaO.01-secondtimer.Thisinstrumenta-tionisdiscussedinmoredetailinreference3.TiresGeneraldescription.-Thetirestestedinthisinvestigationwereapatiof26-inch-diameter,26x 6.6, typeVII,U?
14、-ply-ratingribtreadtireswhichweremadebythesanemsmfacturer.Thespecificationsfor 1thesettiesgivenintableIwereeitherobtainedfromreference4 orbydirectmeasurements.Figure3 showsWlated auddeflatedhalfcrosssectionsforthetwotesttties.Thesecrosssectionswereobtainedfrom “Provided by IHSNot for ResaleNo reprod
15、uction or networking permitted without license from IHS-,-,-NACATN3604plastercaststakenwhenthethebeginningofthetests.betweentheprofilesforthe7ttieswereinanewandunusedconditionatThereappearstobenoappreciable.differencetwotires.Tirewear.-Duringthecourseofthepresentinvestigation,therewasanappreciablepr
16、ogressivechangeinthecross-sectionalshapeofthetiresduetoskiddingandworkingofthetires.Therefore,thechrono-logicalorderinwhichthetestdatawerecollectedmaybeofsomeimpor-tanceintheinterpretationofthedata.Thischronologicalorderisindicatedinthispaperbya seriesletterwhichisassignedtoalltestdata.Specifically,
17、thetestsinchronologicalorderareA,B,C,andD.Thechangeintire-treadpatternduetotirewesrthroughoutthetestisillustratedinfigure4.Atthebeginningofthetestsbothtireshadarectangularcross-sectionaltreadpattern(fig.4(a)andthispat-ternwassubstantiallypreservedthroughoutseriesA (fig.4(b).DuringtetseriesB thesides
18、ofthetreadstidirectcontactwiththewoundbegantowearawayad thiswesringawayproducedthetreadshapeshowninfigure4(c),whichwastakenatthebeginningoftestsertesC. DuringtestseriesCthiswearincreasedsubstantiallyasisshowntifigure4(d)fortireB attheendoftestseriesC. FortestseriesD,forwhichonlytireAwastested,thesma
19、llprojectingedgesremainingonthetreadattheconclusionoftestseriesC (showninfig.4(d)werecutoffbeforebeghninnthetests.(Seefig.4(e).)Itshouldbenotedthat,whenthetireswereremovedfromthetestvehicleattheconclusionofthetests,tireBwasfoundtohavesufferedseverslapparentlydeepcutsarounditsoutboardsidewallinthepro
20、xim-ityofthewheelrhn.ThesecutswereevidentlymadebytheoutboardsideofthewheelrimcuttingintothetireduringoneoftherunsoftestseriesC atthelargeryawanglewherelargeverticalandlateraltiredeflectionswereexperienced.Inordertoinvestigatetheimportanceofthesecuts,thesectionofthetirehavingthedeepestcutwasremovedan
21、dinspected.A photographofthissectionispresentedasfigure4(f).l?romthiscrosssectionitappearedthatthiscutpenetratedcompletelythroughonlyoneplyofthecasingandthereforeprobablydidnotappre-ciablyaffectthetirecharacteristics.Itwasfoundaftercloseexam-inationthattireA hadnotexperiencedthistypeofdamage.Itceeth
22、e radius.-Radius-pressurehysteresisloopsassociatedwithincreasingsmddecreasingpressuresreshowninfigure5 fortiresAandB. Theelapsedtimefromthestat isshownfora fewofthemeamre-mentspresented.Thevariationinthe radiusduetohysteresisforagivenpressureisseentobepracticallynegligible(lessthan0.1inch)intheopera
23、tingpressurerangeforthesetiresforthisrelativelyslowrateofchangeofpressure(roughly,3hoursformostofthecycle).Alsoshowninthisfigureareseveralradiusmeasurementswhichweremadeafterthetireshadbeenleftunloadedatconstantpressureforatleast24hoursinordertoreachanequibriumcondition. . ._ _. _ _ . _Provided by I
24、HSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- . . -8TestSurfaceNACATN3604I.Allyawed-straight-rollinganddragtestswereconductedbytowingthetestvehiclealongthecenterofa 9-inch-thickreinforced-concretetaxistrip.Thistsxistriphada slightcrownsothatthetiresonthetestve
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