DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kwon, Oh Joon | - |
dc.contributor.author | Hah, Chunill | - |
dc.date.accessioned | 2009-06-12T09:50:56Z | - |
dc.date.available | 2009-06-12T09:50:56Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1994-06 | - |
dc.identifier.citation | AIAA Applied Aerodynamics Conference, v., no., pp. - | - |
dc.identifier.issn | 0001-1452 | - |
dc.identifier.uri | http://hdl.handle.net/10203/9367 | - |
dc.description.sponsorship | The 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.language | ENG | - |
dc.language.iso | en_US | en |
dc.publisher | American Institute of Aeronautics and Astronautics | - |
dc.title | Solution of the 3-D Navier-Stokes equations with a two-equation turbulence model on unstructured meshes applied to turbomachinery | - |
dc.type | Conference | - |
dc.type.rims | CONF | - |
dc.citation.publicationname | AIAA Applied Aerodynamics Conference | - |
dc.identifier.conferencecountry | United States | - |
dc.identifier.conferencecountry | United States | - |
dc.contributor.localauthor | Kwon, Oh Joon | - |
dc.contributor.nonIdAuthor | Hah, Chunill | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.