Applications of unstructured hybrid grid method to high-Reynolds number viscous flows

DOI<97::AID-FLD957>3.0.CO;2-D 10.1002/(SICI)1097-0363(19990915)31:1<97::AID-FLD957>3.0.CO;2-DzbMath0986.76052OpenAlexW2007868400MaRDI QIDQ4952988

Dmitri Sharov, Masatoshi Kodera, Kazuhiro Nakahashi, Shintaro Kano

Publication date: 20 February 2001

Full work available at URL: https://doi.org/10.1002/(sici)1097-0363(19990915)31:1<97::aid-fld957>3.0.co;2-d

zbMATH Keywords

Navier-Stokes equationscompressible flowstransonic flowsONERA M6 wingone-equation turbulence modelfinite volume cell-vertex schemeLU-SGS implicit time integration methodONERA M5 airplanescramjet inletsupersonic shock/boundary layer interacting flowsunstructured hybrid grid method

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25) Gas dynamics (general theory) (76N15) Supersonic flows (76J20)

Related Items

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Cites Work

• Interaction between crossing oblique shocks and a turbulent boundarylayer
• Hybrid Prismatic/Tetrahedral Grid Generation for Viscous Flow Applications