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Detailed analysis of a mixed compression hypersonic intake

Koschel, W. and Schneider, A. (1999) Detailed analysis of a mixed compression hypersonic intake. In: Fourteenth International Symposium on Air Breathing Engines. AIAA. XIV ISABE, Florence, Italy; 5-10 September, 1999. ISBN 1-56347-357-7

Full text not available from this repository.

Abstract

An experimental study of the internal shock system of a series of inlet models is presented and discussed. The purpose of this experimental investigation was to evaluate the possibilities of influencing the shock/shock and shock/boundary layer interaction by the design of a suitable inlet geometry and thus avoiding bleed systems. In particulr, the occurrence of boundary layer separation was investigated. The wall pressure distribution is measured and compared to numerical results of CFD calculations. Another test series deals with the start behavior of the internal compression section of the mixed compression inlet. Therefore the development of the shock structure during intake start phases was investigated using a color-schlieren system and video recording. The air flow in the test section was slowly accelerated from zero to Mach 3.0, and the shock system was recorded.

Item URL in elib:https://elib.dlr.de/1411/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999, monograph_id=ISABE 79-7036,
Title:Detailed analysis of a mixed compression hypersonic intake
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Koschel, W.UNSPECIFIEDUNSPECIFIED
Schneider, A.RWTH AachenUNSPECIFIED
Date:1999
Journal or Publication Title:Fourteenth International Symposium on Air Breathing Engines
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmail
International Society for Air Breathing Engines (ISABE), UNSPECIFIED
Publisher:AIAA
ISBN:1-56347-357-7
Status:Published
Event Title:XIV ISABE, Florence, Italy; 5-10 September, 1999
Organizer:ISOABE
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):E - no assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Lohmiller, Monika
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:44

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