elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | 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: Proceedings of the ASME TURBO EXPO 2008, Vol 4, Pts A and B, 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.

Abstract

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.

Item URL in elib:https://elib.dlr.de/57142/
Document Type:Conference or Workshop Item (Speech)
Title:Characterization of Advanced Combustor Cooling Concepts under Realistic Operating Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Behrendt, ThomasUNSPECIFIEDUNSPECIFIED
Lengyel, TimeaUNSPECIFIEDUNSPECIFIED
Hassa, ChristophUNSPECIFIEDUNSPECIFIED
Gerendas, MiklosRolls-Royce DeutschlandUNSPECIFIED
Date:9 June 2008
Journal or Publication Title:Proceedings of the ASME TURBO EXPO 2008, Vol 4, Pts A and B
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Page Range:GT2008-51191
Publisher:ASME
ISBN:0-7918-3824-2
Status:Published
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
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Combustion Chamber Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Combustor
Deposited By: Behrendt, Dr.-Ing. Thomas
Deposited On:07 Jan 2009
Last Modified:27 Jun 2018 11:19

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.