DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Characterization of Advanced Combustor Cooling Concepts under Realistic Operating Conditions

Behrendt, Thomas and Lengyel, Timea and Hassa, Christoph and Gerendas, Miklos (2008) Characterization of Advanced Combustor Cooling Concepts under Realistic Operating Conditions. In: Proc. of ASME Turbo Expo 2008, GT2008-51191. ASME. ASME Turbo Expo, 2008-06-09 - 2008-06-13, Berlin, Deutschland. ISBN 0-7918-3824-2.

Full text not available from this repository.


For future low emission aero engine combustors a significant reduction of cooling air consumption is required. Quantitative data of the performance of advanced cooling concepts in a realistic environment in addition to existing data from scaled isothermal investigations is needed by combustor designers for further improvements. The effect of the cooling air properties on the cooling effectiveness of different advanced cooling concepts at realistic operating conditions is analyzed. Adapting of the measuring techniques and correction of the exhaust gas radiation will be especially addressed. An introduction into basic cooling design considerations is included.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Characterization of Advanced Combustor Cooling Concepts under Realistic Operating Conditions
AuthorsInstitution or Email of Authors
Behrendt, ThomasUNSPECIFIED
Hassa, ChristophUNSPECIFIED
Gerendas, MiklosRolls-Royce Deutschland
Date:9 June 2008
Journal or Publication Title:Proc. of ASME Turbo Expo 2008
Refereed publication:Yes
In ISI Web of Science:No
Page Range:GT2008-51191
Keywords:Combustor, effusion cooling, IR thermography, heat transfer
Event Title:ASME Turbo Expo
Event Location:Berlin, Deutschland
Event Type:international Conference
Event Dates:2008-06-09 - 2008-06-13
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 - Combustion Chamber Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Combustor
Deposited By: Dr.-Ing. Thomas Behrendt
Deposited On:07 Jan 2009
Last Modified:27 Apr 2009 15:40

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.