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Design of a generic subsonic S-duct intake for studies on the effect of boundary layer ingestion

Rein, Martin and Hannemann, Monika and Gardner, Anthony and Koch, Stefan (2009) Design of a generic subsonic S-duct intake for studies on the effect of boundary layer ingestion. DLR-Interner Bericht. DLR-IB 224-2009 A28, 30 S.

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Abstract

Topic of the present report is the design of a generic model of a highly integrated intake. The model is planned for an experimental study of the combined effects of boundary layer ingestion and an S-duct diffuser on flow conditions at the engine face. In order to form a well-defined boundary layer ahead of the intake the model is arranged on a flat plate. In the introduction the importance of boundary layer ingesting highly integrated intakes is briefly discussed. This is followed by basic theoretical considerations and a detailed description of the analytical design. Preliminary computational results of the flow field within the intake performed with DLR’s Tau code are presented next. Finally, the experimental procedure to be used in the experiments that shall be performed in the cryogenic blow down tunnel Göttingen (KRG) of the German-Dutch Wind Tunnels DNW is outlined. The report is closed by an outlook.

Item URL in elib:https://elib.dlr.de/60239/
Document Type:Monograph (DLR-Interner Bericht)
Title:Design of a generic subsonic S-duct intake for studies on the effect of boundary layer ingestion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rein, Martinmartin.reinUNSPECIFIED
Hannemann, Monikamonika.hannemann (at) dlr.deUNSPECIFIED
Gardner, Anthonyanthony.gardner (at) dlr.dehttps://orcid.org/0000-0002-1176-3447
Koch, Stefanstefan.koch (at) dlr.deUNSPECIFIED
Date:2009
Journal or Publication Title:Institutsbericht
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Volume:IB 224
Number of Pages:30
Editors:
EditorsEmail
Deutsches Zentrum für Luft- und Raumfahrt, e.V.UNSPECIFIED
Series Name:Institutsbericht
Keywords:intake, S-duct intake, boundary layer ingestion
Institution:DLR, Institute of Aerodynamics and Flow Technology
Department:High-Speed Configurations
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Military Technologies (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Rein, Prof.Dr. Martin
Deposited On:29 Oct 2009 15:05
Last Modified:01 Dec 2018 19:46

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