基于彻体力模型的进气道与压气机一体化模拟

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中图分类号：V231.3 文献标志码：B 文章编号：1671-5276（2025）06-0145-05

Abstract：Basedontheideaofthebodyforce model，thecompressorismodeledandreduced，andtheintegratedcalculationof theinletandtheompressorisrealized，therebyreducingthedemandforcomputingresourcesintheintegratedcalculationand analysisprocessof theinletandthecompresor.Through theexchangeof numerical transferandboundaryconditions between three-dimensionalRANScalculationandbodyforcecalculation，theintegratedcalculationmodelisconstructed，withwhichthe couplingiscalculatedbetweenanS-shaped-nletandafanrotor.Theresultsshowthatthecalculationmodelcapturesthetypical flowfieldcharacteristicsoftheS-shaped-inletoutletandtheinfluenceoftheinletoutletflowfielddistortiononthecopressor performance，whichverifiesthefeasibilityofthecalculationmodel.Itisofengineeringsignificancetopredicttheinteraction between the inlet and the compressor in the early stage of the propulsion system design.

Keywords：aeroengine；inlet-enginematching；inletcompresorintegration；three-dimensionalbodyforcemodel inlet distortion

0 引言

压气机作为航空燃气涡轮发动机的重要部件，主要对气体起到做功增压的作用，由其工作特点所决定，压气机中的气体流动通常是强逆压力梯度的，这就导致其具有气动失稳特性。（剩余5425字）