3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Weber, A. and Schreiber, H. A. and Fuchs, R. and Steinert, W. (2002) 3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall. ASME Journal of Turbomachinery, Vo. 124, July 2002, pp. 358-366.

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Item URL in elib:

https://elib.dlr.de/1314/

Document Type:

Article

Additional Information:

LIDO-Berichtsjahr=2005,

Title:

3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Weber, A.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Schreiber, H. A.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Fuchs, R.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Steinert, W.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2002

Journal or Publication Title:

ASME Journal of Turbomachinery

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Yes

Volume:

Vo. 124, July 2002

Page Range:

pp. 358-366

Status:

Published

Keywords:

Transonic compressor flow, 3-D test case

HGF - Research field:

Aeronautics, Space and Transport (old)

HGF - Program:

Aeronautics

HGF - Program Themes:

other

DLR - Research area:

Aeronautics

DLR - Program:

L TT - Triebwerkstechnologien

DLR - Research theme (Project):

L - Fan and Compressor Technologies (old)

Location:

Köln-Porz

Institutes and Institutions:

Institute of Propulsion Technology

Deposited By:

Schreiber, Herr Heinz-Adolf

Deposited On:

16 Sep 2005

Last Modified:

06 Jan 2010 13:36

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