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Numerical Investigation of a 4.5-stage Compressor with Variable Geometry

Keil, Markus (2015) Numerical Investigation of a 4.5-stage Compressor with Variable Geometry. Master's. DLR-Interner Bericht. DLR-IB 325-06-15, 101 S.

Full text not available from this repository.

Abstract

Calculation of the DLR Rig250 at different settings of the variable stator vanes in order to reproduce the roll-over experiments.

Item URL in elib:https://elib.dlr.de/96376/
Document Type:Monograph (DLR-Interner Bericht, Master's)
Title:Numerical Investigation of a 4.5-stage Compressor with Variable Geometry
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Keil, MarkusAT-FUVUNSPECIFIED
Date:June 2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:101
Status:Published
Keywords:roll-over, compressor, variable stator vane
Institution:Technische Universität Darmstadt
Department:Fachbereich Maschinenbau,
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
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Reutter, Oliver
Deposited On:10 Jun 2015 11:47
Last Modified:10 Jun 2015 11:47

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