Solution of the 3-D Navier-Stokes equations with a two-equation turbulence model on unstructured meshes applied to turbomachinery

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dc.contributor.authorKwon, Oh Joon-
dc.contributor.authorHah, Chunill-
dc.date.accessioned2009-06-12T09:50:56Z-
dc.date.available2009-06-12T09:50:56Z-
dc.date.created2012-02-06-
dc.date.issued1994-06-
dc.identifier.citationAIAA Applied Aerodynamics Conference, v., no., pp. --
dc.identifier.issn0001-1452-
dc.identifier.urihttp://hdl.handle.net/10203/9367-
dc.description.sponsorshipThe authors would like to express their indebtedness to Dr. Neal T. Frink at NASA Langley for his help and encouragement during the course of the present work. Chris J. Steffen at NASA Lewis is also appreciated for technical discussions and for providing experimental data and structured grid results for the backward-facing step flow.en
dc.languageENG-
dc.language.isoen_USen
dc.publisherAmerican Institute of Aeronautics and Astronautics-
dc.titleSolution of the 3-D Navier-Stokes equations with a two-equation turbulence model on unstructured meshes applied to turbomachinery-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationnameAIAA Applied Aerodynamics Conference-
dc.identifier.conferencecountryUnited States-
dc.identifier.conferencecountryUnited States-
dc.contributor.localauthorKwon, Oh Joon-
dc.contributor.nonIdAuthorHah, Chunill-

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