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

Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part I: Principal Cascade Design and Compressor Application

Dorfner, Christian and Hergt, Alexander and Nicke, Eberhard and Mönig, Reinhard (2011) Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part I: Principal Cascade Design and Compressor Application. Journal of Turbomachinery, Vol. 133 (021026), pp. 1-6. DOI: DOI: 10.1115/1.4001223.

Full text not available from this repository.


Document Type:Article
Title:Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part I: Principal Cascade Design and Compressor Application
Authors:
AuthorsInstitution or Email of Authors
Dorfner, ChristianEADS
Hergt, AlexanderDLR
Nicke, EberhardDLR
Mönig, ReinhardDLR
Date:2011
Journal or Publication Title:Journal of Turbomachinery
Refereed publication:Yes
In Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:Vol. 133
DOI:DOI: 10.1115/1.4001223
Page Range:pp. 1-6
Status:Published
Keywords:Non-Axisymetric Endwall Contour, Secondary Flow, Axial Compressor
HGF - Research field:Aeronautics, Space and Transport
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 > Fan and Compressor Technology
Institute of Propulsion Technology > Fan and Compressor
Deposited By: Alexander Silvio Hergt
Deposited On:17 Nov 2011 08:22
Last Modified:04 Apr 2013 16:32

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.