DETAILED FLOW ANALYSIS OF A COMPRESSOR CASCADE WITH A NON-AXISYMMETRIC ENDWALL CONTOUR

Hergt, Alexander and Klinner, Joachim and Steinert, Wolfgang and Dorfner, Christian and Nicke, Eberhard (2011) DETAILED FLOW ANALYSIS OF A COMPRESSOR CASCADE WITH A NON-AXISYMMETRIC ENDWALL CONTOUR. 9th ETC , 21.-25. March, 2011, Istanbul, Turkey.

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Item URL in elib:

https://elib.dlr.de/71629/

Document Type:

Conference or Workshop Item (Speech, Paper)

Title:

DETAILED FLOW ANALYSIS OF A COMPRESSOR CASCADE WITH A NON-AXISYMMETRIC ENDWALL CONTOUR

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD
Hergt, Alexander	DLR	UNSPECIFIED
Klinner, Joachim	DLR	UNSPECIFIED
Steinert, Wolfgang	DLR	UNSPECIFIED
Dorfner, Christian	EADS	UNSPECIFIED
Nicke, Eberhard	DLR	UNSPECIFIED

Date:

March 2011

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

Non-axisymetric Endwall Contour, Secondary Flow, Compressor Cascade

Event Title:

9th ETC

Event Location:

Istanbul, Turkey

Event Type:

international Conference

Event Dates:

21.-25. March, 2011

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 08:23

Last Modified:

17 Nov 2011 08:23

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