摘要
Anewlydesignedstrutisproposedinthispaperforfuelinjectionandflameholdinginaliquid-kerosene-fueledsupersoniccombustor.Thethicknessofthestrutis8mmandthefrontblockageisabout8%.Thecharacteristicofthisstrutisthatextraoxygencanbeinjectedthroughasetoforificesatthebackofthestrut,whichcanchangethelocalflowfieldstructureandER(EquivalenceRatio).Basedontheabovementionedstrut,astablelocalflameisgeneratedatthebackofthestrutandthemaincombustioncanbeorganizedaroundthislocalfire.Numericalsimulationisconductedtocomparethelocalflowfielddistributionatthebackofthestrutwith/withoutextraoxygeninjection.Experimentsareconductedtotestthecombustioncharacteristicsbasedonthisfuelinjectionandflameholdingstrategy.Thetemperaturedistributionwhichcanreflectthelocalflamecharacteristichasbeenmeasuredintheexperimentsconductedundercoldincomingsupersonicairflowcondition.Inaddition,theoverallcombustionperformanceinafull-scalesupersoniccombustorhasbeenevaluatedintheexperimentsconductedunderhotincomingsupersonicairflowcondition.Resultsshowthatthisstrutstrategyisverypromisingsinceitcanorganizestablesupersoniccombustionatthecenterofthecombustorwithoutanycavityorrearwardfacingstep.Besidesthat,evenwiththe8mmthickstrut,thecombustioncanbestableinawiderangeofERfrom0.25-1byusingliquidroom-temperaturekerosene.
出版日期
2013年05月15日(中国期刊网平台首次上网日期,不代表论文的发表时间)