elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

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.

Full text not available from this repository.


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 Authors
Franjou, CarlUNSPECIFIED
Date:August 2006
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
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Rosemarie Fox
Deposited On:22 Aug 2006
Last Modified:27 Apr 2009 13:01

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.