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Validation of an Acoustically 3-D-Designed Turbine Exit Guide Vane

Broszat, D. and Kennepohl, F. and Tapken, U. and Möser, M. and Heitmeir, F. (2010) Validation of an Acoustically 3-D-Designed Turbine Exit Guide Vane. In: Proceedings 16th AIAA/CEAS Aeroacoustics Conference (AIAA Paper Nr.: 2010-3806). Curran Associates, Inc.. 16th AIAA/CEAS Aeroacoustics Conference, 07.-09. Juni 2010, Stockholm, Schweden. ISBN 9781617388545.

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Document Type:Conference or Workshop Item (Paper)
Title:Validation of an Acoustically 3-D-Designed Turbine Exit Guide Vane
Authors:
AuthorsInstitution or Email of Authors
Broszat, D.MTU Aero Engines GmbH, München
Kennepohl, F.MTU Aero Engines GmbH, München
Tapken, U.UNSPECIFIED
Möser, M.Institut für Thermische Turbomaschinen und Maschinendynamik, TU Graz
Heitmeir, F.Institut für Thermische Turbomaschinen und Maschinendynamik, TU Graz
Date:2010
Journal or Publication Title:Proceedings 16th AIAA/CEAS Aeroacoustics Conference
Refereed publication:Yes
In ISI Web of Science:No
Publisher:Curran Associates, Inc.
ISBN:9781617388545
Status:Published
Keywords:Aeroacoustics Conference, CEAS, Turbine
Event Title:16th AIAA/CEAS Aeroacoustics Conference
Event Location:Stockholm, Schweden
Event Type:international Conference
Event Dates:07.-09. Juni 2010
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies
Location: Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Balbir Kaur
Deposited On:01 Feb 2011 11:49
Last Modified:01 Feb 2011 11:49

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