Hoheisel, H. und Bütefisch, K.-A. und Lehmann, B. und Henke, R. und Roscher, H.J. Seelhorst, U., (1992) "THE JET BEHAVIOUR OF AN HIGH-BYPASS ENGINE AS DETERMINED BY LDA-MEASUREMENTS IN GROUND TESTS". AGARD Conference Proceedings 498 Aerodynamic Engine/Airframe Integration for High Performance Aircraft and Missiles Fluid Dynamics Panel Symposium held in Fort Worth, Texas, US 7th - 10th October, 1991.
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Kurzfassung
The present contribution describes the measurements of a three-component LDA within the jet of a bypass engine CFM56-5 installed on an A320, in the form of ground tests. The aerodynamic data obtained at the fan exit and in tweo sections at the turbine nozzle exit near cruise condition allow an insight into the complete jet behaviour. The velocity components in the specified position for all three coordinate directions are discussed allowing the evaluationof the radial velocity distribution and the swirl components. In addition, the important paramters of the turbulence intensity and the direction of the thrust vector are considered.
elib-URL des Eintrags: | https://elib.dlr.de/36943/ | ||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||||||||||||||
Zusätzliche Informationen: | LIDO-Berichtsjahr=1992, pages=8, | ||||||||||||||||||||||||
Titel: | "THE JET BEHAVIOUR OF AN HIGH-BYPASS ENGINE AS DETERMINED BY LDA-MEASUREMENTS IN GROUND TESTS" | ||||||||||||||||||||||||
Autoren: |
| ||||||||||||||||||||||||
Datum: | 1992 | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | Engine Integration, Flow Field Measurement, Thrust, Vector, Three Component LDA | ||||||||||||||||||||||||
Veranstaltungstitel: | AGARD Conference Proceedings 498 Aerodynamic Engine/Airframe Integration for High Performance Aircraft and Missiles Fluid Dynamics Panel Symposium held in Fort Worth, Texas, US 7th - 10th October, 1991 | ||||||||||||||||||||||||
HGF - Forschungsbereich: | NICHT SPEZIFIZIERT | ||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | keine Zuordnung | ||||||||||||||||||||||||
DLR - Schwerpunkt: | NICHT SPEZIFIZIERT | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | L SI - Versuchs- und Simulationstechniken | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | NICHT SPEZIFIZIERT | ||||||||||||||||||||||||
Standort: | Köln-Porz , Braunschweig , Göttingen | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik | ||||||||||||||||||||||||
Hinterlegt von: | DLR-Beauftragter, elib | ||||||||||||||||||||||||
Hinterlegt am: | 03 Apr 2006 | ||||||||||||||||||||||||
Letzte Änderung: | 27 Apr 2009 10:07 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags