飞机总体方案设计例子.doc

该【飞机总体方案设计例子 】是由【ATONGMU】上传分享，文档一共【205】页，该文档可以免费在线阅读，需要了解更多关于【飞机总体方案设计例子 】的内容，可以使用淘豆网的站内搜索功能，选择自己适合的文档，以下文字是截取该文章内的部分文字，如需要获得完整电子版，请下载此文档到您的设备，方便您编辑和打印。=PreliminaryDesignReviewAAE451AircraftDesignFinalReportTeamV27April,2006StephenBeirneCharlieRushMilesHatemZhengWangChrisKesterBrandonWeddeJimRadtkeGregWilsonTeamV;2ExecutiveSummaryTheBarnOwlisTeamV’-oilapproachesandpetroleum--termneedforareplacementfor100octanelow---termmarkethasbeenestimatedatover$1billionannuallyonce100low-,--weightdesignwasselectedfromthefeasiblespace,--,-,-the-$278,’;3TableofContentsIntroduction.........................................................................................................................................4DesignRequirements.........................................................................................................................5ProposedConcept...............................................................................................................................6DesignMission.....................................................................................................................................7Sizing.....................................................................................................................................................82DAerodynamics..............................................................................................................................193DAerodynamics..............................................................................................................................24Performance......................................................................................................................................31Structures...........................................................................................................................................35WeightandBalance&Stability.....................................................................................................50Propulsion..........................................................................................................................................55Cost.....................................................................................................................................................parisons...............................................................................................................72References..........................................................................................................................................75AppendixA–AdditionalBarnOwlPictures...............................................................................76AppendixB–Sizing/CarpetPlotCode.........................................................................................79AppendixC–DragPolarData.......................................................................................................87AppendixD–WingStructureOptimizationCode.....................................................................88AppendixE–WingOptimizationCodeOutputs........................................................................96AppendixF–EmptyWeightCalculationCode..........................................................................99AppendixG–AluminumEquivalentInputsforAppendixC.................................................101AppendixH–FiberglassPropertyCalculationCode................................................................102AppendixI–V-nDiagramCode..................................................................................................105AppendixJ–FlightEnvelopeCode............................................................................................107TeamV;4IntroductionThisteam’ssystemrequirementsreview[14]describedaplantotargetthegeneralaviationmarketwithasingle-engine,four-seataircraft–,fixedbaseoperators,andtrainingfleetsinthephase-outof100octanelow-lead(100LL)aviationgasolineandthetransitionaltimesof“peak-oil.”,ormore,couldbeexpectedinthewakeofthe100LLphase-[13].Bio--wing,;5DesignRequirementsThecurrentdesignrequirementsshownbelowinTable1arestillthesameaspresentedinthisteam’sSystemDefinitionReview[13].Throughtheworkpresentedinthisreport,itwillbeshownthatatthecurrentlevelofdetailanalternate--DesignRequirementsDesignRequirementsSummary?1500fttakeoffdistancetocleara50ftobstacle?600lbpayloadwithmaxfuel?125ktsmaxcruisespeed,Target=150kts?500nmrange,Target=600nm?48x44cabinheightxwidthTargetGTOWof2800lbsTargetbasepriceof$300,000TeamV;6ProposedConceptTeamV’,conventionaltail,singleengine,tractorprop,-Concept3ViewTeamV;7DesignMissionBaseduponthisteam’sQFDanalysis,aspresentedinthesystemrequirementsreview,–DesignMissionTable2–DesignMissionLegendATaxi14minutesFClimbtodivertaltitude(2000ftMSL)BTake-offrollatsealevelG45-minloiter/divertCClimbtocruise(8000ftMSL),,,itwillthenclimbtoadivert/,land,;8Sizing