dc.contributorUniversidade de São Paulo (USP)
dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2018-12-11T16:39:07Z
dc.date.available2018-12-11T16:39:07Z
dc.date.created2018-12-11T16:39:07Z
dc.date.issued2015-01-01
dc.identifierProcedia IUTAM, v. 14, p. 374-380.
dc.identifier2210-9838
dc.identifierhttp://hdl.handle.net/11449/167983
dc.identifier10.1016/j.piutam.2015.03.063
dc.identifier2-s2.0-84940656168
dc.description.abstractIn practical situations, natural transition determines the transition to turbulence process. Experimental evidence suggest that the wave packet evolution is related closely to natural transition. The major part of numerical works on wave packets are focused on incompressible, supersonic and hypersonoc flows, subsonic ones are probably the less researched. A compressible DNS code was developed, several code validation tests were performed, including a simulation of an experiment of wave packets 1. The evolution of wave packets on compressible boundary layer in a flat plate is studied by Direct Numerical Simulations (DNS), to investigate the effect of Mach number in the initial nonlinear stages. For Mach 0.9 were considered three cases: linear, nonlinear and interaction between two packets. Results suggest that subharmonic mechanism is the most probable scenario at the initial nonlinear stages.
dc.languageeng
dc.relationProcedia IUTAM
dc.relation0,254
dc.rightsAcesso aberto
dc.sourceScopus
dc.subjectCompressible boundary layer
dc.subjectDNS simulation
dc.subjectnatural transition
dc.subjectsubsonic boundary layer
dc.subjectwave packet
dc.titleWavepackets in Boundary Layers Close to Transonic Speeds
dc.typeActas de congresos


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