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Flow field mixing characteristics of an aero-engine combustor - Part 1: Experimental results

Hassa, C. and Voigt, P. and Lehmann, B. and Schodl, R: and Carl, M. and Ripplinger, T: and Zarzalis, M. (2002) Flow field mixing characteristics of an aero-engine combustor - Part 1: Experimental results. 38th IAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis (US), 7-10 July, 2002.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003, monograph_id=2002-3709,
Title:Flow field mixing characteristics of an aero-engine combustor - Part 1: Experimental results
Authors:
AuthorsInstitution or Email of Authors
Hassa, C.UNSPECIFIED
Voigt, P.UNSPECIFIED
Lehmann, B.UNSPECIFIED
Schodl, R:UNSPECIFIED
Carl, M.UNSPECIFIED
Ripplinger, T:UNSPECIFIED
Zarzalis, M.UNSPECIFIED
Date:2002
Editors:
EditorsEmail
AIAA, UNSPECIFIED
Series Name:AIAA paper No. AIAA-2002-3709
Status:Published
Keywords:aero-engine combustor
Event Title:38th IAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis (US), 7-10 July, 2002
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 - Virtual Engine and Validation Methods
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By:INVALID USER
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:21

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