A Method for Efficient Performance Prediction for Fan and Compressor Stages with Degraded Blades

Giebmanns, Angela and Schnell, Rainer and Werner-Spatz, Christian (2015) A Method for Efficient Performance Prediction for Fan and Compressor Stages with Degraded Blades. ASME Turbo Expo 2015, 2015-06-15 - 2015-06-19, Montréal, Kanada. doi: 10.1115/GT2015-42108.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/101346/

Document Type:

Conference or Workshop Item (Speech)

Title:

A Method for Efficient Performance Prediction for Fan and Compressor Stages with Degraded Blades

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Giebmanns, Angela	DLR-AT	UNSPECIFIED	UNSPECIFIED
Schnell, Rainer	DLR-AT	UNSPECIFIED	UNSPECIFIED
Werner-Spatz, Christian	Lufthansa Technik AG	UNSPECIFIED	UNSPECIFIED

Date:

June 2015

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

DOI:

10.1115/GT2015-42108

Status:

Published

Keywords:

MRO, beschädigte Schaufel, Fan, Verdichter, Schaufelgeometrie, CFD, adjungierter Strömungslöser, Leistungsvorhersage

Event Title:

ASME Turbo Expo 2015

Event Location:

Montréal, Kanada

Event Type:

international Conference

Event Start Date:

15 June 2015

Event End Date:

19 June 2015

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:

Giebmanns, Angela

Deposited On:

05 Jan 2016 08:17

Last Modified:

24 Apr 2024 20:06

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