THE EFFECT OF AN ERODED LEADING EDGE ON THE AERODYNAMIC PERFOMANCE OF A TRANSONIC FAN BLADE CASCADE

Hergt, Alexander and Klinner, Joachim and Steinert, Wolfgang and Grund, Sebastian and Giebmanns, Angela and Schnell, Rainer (2014) THE EFFECT OF AN ERODED LEADING EDGE ON THE AERODYNAMIC PERFOMANCE OF A TRANSONIC FAN BLADE CASCADE. In: ASME Turbo Expo. ASME Turbo Expo, 16.-20. Juni 2014, Düsseldorf, Germany.

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Item URL in elib:

https://elib.dlr.de/90604/

Document Type:

Conference or Workshop Item (Speech)

Additional Information:

GT2014-25023

Title:

THE EFFECT OF AN ERODED LEADING EDGE ON THE AERODYNAMIC PERFOMANCE OF A TRANSONIC FAN BLADE CASCADE

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD
Hergt, Alexander	UNSPECIFIED	UNSPECIFIED
Klinner, Joachim	UNSPECIFIED	UNSPECIFIED
Steinert, Wolfgang	DLR-AT	UNSPECIFIED
Grund, Sebastian	DLR-AT	UNSPECIFIED
Giebmanns, Angela	DLR-AT	UNSPECIFIED
Schnell, Rainer	AT-FUV	UNSPECIFIED

Date:

June 2014

Journal or Publication Title:

ASME Turbo Expo

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Yes

Status:

Published

Keywords:

Eroded leading edge

Event Title:

ASME Turbo Expo

Event Location:

Düsseldorf, Germany

Event Type:

international Conference

Event Dates:

16.-20. Juni 2014

Organizer:

ASME

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 (old)

Location:

Köln-Porz

Institutes and Institutions:

Institute of Propulsion Technology > Fan and Compressor

Deposited By:

Hergt, Dr.-Ing. Alexander Silvio

Deposited On:

16 Sep 2014 15:04

Last Modified:

09 Feb 2017 19:20

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