Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

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. DOI: DOI: 10.1115/1.4001224.

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Document Type:

Article

Title:

Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Authors:

Authors	Institution or Email of Authors
Hergt, Alexander	DLR
Dorfner, Christian	EADS
Steinert, Wolfgang	DLR
Nicke, Eberhard	DLR
Schreiber, Heinz-Adolf	DLR

Date:

2011

Journal or Publication Title:

Journal of Turbomachinery

Refereed publication:

Yes

In Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

Volume:

Vol. 133

DOI:

DOI: 10.1115/1.4001224

Page Range:

pp. 1-8

Status:

Published

Keywords:

Non-Axisymetric Endwall Contour, Secondary Flow, Compressor Cascade

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

L ER - Engine Research

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

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