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Analysis of the 3 dimensional flow in an axial compressor stage with a highly loaded stator by using Computational Fluid Dynamics.

Franjou, Carl (2006) Analysis of the 3 dimensional flow in an axial compressor stage with a highly loaded stator by using Computational Fluid Dynamics. Diploma. DLR-Interner Bericht.

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Item URL in elib:https://elib.dlr.de/44511/
Document Type:Monograph (DLR-Interner Bericht, Diploma)
Title:Analysis of the 3 dimensional flow in an axial compressor stage with a highly loaded stator by using Computational Fluid Dynamics.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Franjou, CarlUNSPECIFIEDUNSPECIFIED
Date:August 2006
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:81
Status:Published
Keywords:axial compressor, 3D Navier Stokes, grid refinement
Institution:ESTACA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Fox, Rosemarie
Deposited On:22 Aug 2006
Last Modified:27 Apr 2009 13:01

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