Hergt, Alexander and Dorfner, Christian and Steinert, Wolfgang and Nicke, Eberhard and Schreiber, Heinz-Adolf (2011) Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation. Journal of Turbomachinery, Vol. 133 (021027), pp. 1-8. American Society of Mechanical Engineers (ASME). doi: DOI: 10.1115/1.4001224.
Full text not available from this repository.
Item URL in elib: | https://elib.dlr.de/71633/ | ||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Document Type: | Article | ||||||||||||||||||
Title: | Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation | ||||||||||||||||||
Authors: |
| ||||||||||||||||||
Date: | 2011 | ||||||||||||||||||
Journal or Publication Title: | Journal of Turbomachinery | ||||||||||||||||||
Refereed publication: | Yes | ||||||||||||||||||
Open Access: | No | ||||||||||||||||||
Gold Open Access: | No | ||||||||||||||||||
In SCOPUS: | Yes | ||||||||||||||||||
In ISI Web of Science: | Yes | ||||||||||||||||||
Volume: | Vol. 133 | ||||||||||||||||||
DOI : | DOI: 10.1115/1.4001224 | ||||||||||||||||||
Page Range: | pp. 1-8 | ||||||||||||||||||
Publisher: | American Society of Mechanical Engineers (ASME) | ||||||||||||||||||
Status: | Published | ||||||||||||||||||
Keywords: | Non-Axisymetric Endwall Contour, Secondary Flow, Compressor Cascade | ||||||||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||
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 > Fan and Compressor Technology Institute of Propulsion Technology > Fan and Compressor | ||||||||||||||||||
Deposited By: | Hergt, Dr.-Ing. Alexander Silvio | ||||||||||||||||||
Deposited On: | 17 Nov 2011 08:22 | ||||||||||||||||||
Last Modified: | 08 Mar 2018 18:46 |
Repository Staff Only: item control page