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时间:2019-03-14
《Comparative Study of Corrosion–Fatigue in Aircraft Materials.pdf》由会员上传分享,免费在线阅读,更多相关内容在学术论文-天天文库。
1、http://www.paper.edu.cnAIAAJOURNALVol.39,No.2,February2001ComparativeStudyofCorrosion–FatigueinAircraftMaterialsQ.Y.Wang,¤R.M.Pidaparti,†andM.J.Palakal‡IndianaUniversity–PurdueUniversityatIndianapolis,Indianapolis,Indiana46202Corrosion–fatigueisoneofthedamagemechanismsaffectingthestructur
2、alintegrityoftheagingaircraft.Simpleanalyticalandprobabilisticmodelsforpredictingpittingcorrosionandcorrosion–fatiguelifeinaluminumalloy2024/T3usedinaircraftstructuresispresented.Thedevelopedmodelincludestheeffectoftheinteractionofcyclicloadandthecorrosiveenvironmentonthefatiguelife,andco
3、nsidersallstagesofthecorrosion–fatigueprocess.Theprobabilisticmodelinvestigatedconsiderstheuncertaintiesininitialpitsize,corrosionpittingcurrent,andmaterialpropertiesduetoscatterfoundintheexperimentaldata.Theanalyticalmodelshowsverygoodquantitativeagreementwiththeexistingexperimentaldataa
4、ndanalyticalmodelsoverawiderangeofparameters.Theresultspredictedthatthecrackinitiationlifevariesapproximately10–40%ascomparedtocrackpropagationlifeincorrosion–fatigueproblems.I.Introductiononsetofcrackgrowth.Inaseriesofpapers,Weietal.4andHarlowandWei5¡7havedevelopedaprobabilisticmodelfort
5、hepredictionATIGUEfailuresmayresultwhenagingaircraftareoperatedinFacorrosiveenvironmentduetonucleation,initiation,andprop-ofcorrosionandcorrosion–fatiguelife.Theirmodelisbasedonagationofcracksatthecorrosionpitsinaircraftmaterials.Scheduledthegrowthofasingledominantawfromapittoasmallsurfac
6、emaintenanceandinspectionofaircraftcomponentsinadvancemaycrackandthenintoathroughcrack.Theyshowedthatprobabilisticpreventsuchfailures.Establishmentofsimpleanalyticalmodelsconceptscouldbeemployedtopredictthepittingcorrosion–fatigueforcorrosion–fatigueishelpfulindesigningamaintenancepro-pro
7、cess.However,intheirmodel,fatiguecracknucleationwasnotconsidered.Rokhlinetal.8developedafracturemechanicsmodelgrambasedontheresiduallifetoavoidfailure.ItiswellknownthatcorrosionpittinghasastrongeffectonfatiguelifeofAlalloysusedforfatiguecrackinitiationandpropagation
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