摘要
TheconceptofusingbladeslottingtosuppressthelargeboundarylayerseparationofhighaerodynamicloadinglowpressureturbineprofilehasbeendevelopedinPart1.Calculatedresultshighlighttheinabilityperformanceaccompaniedwithun-properbladeslottingathighReynoldsnumber,bladeslottingoptimizationseemslikecompulsory.Meanwhile,tofurtherdignifytherationalforuseofbladeslotting,slottingpositionanditsgeometryneededtobeoptimized.Comparisonofdifferentslottingschemecalculationresultspromisedthatbladeslottingparameterlikeoutletangleandoutletpositionarethemostimportantparameterswhichmustbeinvestigatedtosatisfythedesignpurpose.
出版日期
2011年01月11日(中国期刊网平台首次上网日期,不代表论文的发表时间)