摘要
Whennon-equilibriumcondensationoccursinasupersonicflowfield.theflowisaffectedbythelatentheatreleased.Inthepresentstudy.inordertocontrolthetransonicflowfieldwithshockwave,acondensingflowwasproducedbyanexpansionofmoistaironacircularbumpmodelandshockwaveswereoccurredinthesupersonicpartsofthefields.Furthermore,theadditionalpassivetechniqueofshock/boundarylayerinteractionusingtheporouswallwithacavityunderneathwasadoptedinthisflow.Theeffectsofthesemethodsontheshockwavecharacteristicswereinvestigatednumericallyandexperimentally.Theresultobtainedshowedthatthetotalpressurelossintheflowfieldsmightbeeffectivelyreducedbythesuitablecombinationbetweennon-equilibriumcondensationandthepositionofporouswall.
出版日期
2003年02月12日（中国期刊网平台首次上网日期，不代表论文的发表时间）
