Wagner, Bernd und Stark, Ralf (2009) Experimental Study of a Planar Expansion-Deflection Nozzle. 3RD EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS), 2009-07-06 - 2009-07-09, Versailles/Paris, Frankreich.
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Kurzfassung
A planar expansion-deflection nozzle was tested on the cold flow test bench P6.2 at DLR Lampoldshausen. The comparison between experimental data, design, and numerical results at the design point show a good agreement in general with a slight deviation due to a higher expansion in the experiments. The wake closure was investigated on transient pressure profiles. A hysterisis is existing in these experiments for the transition from open to closed operation mode and back. For low pressure ratios in the off design region, flow separation on the center body was observed. The separation shock interacts with the outer contour leading to pressure peaks.
elib-URL des Eintrags: | https://elib.dlr.de/62750/ | ||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||
Titel: | Experimental Study of a Planar Expansion-Deflection Nozzle | ||||||||||||
Autoren: |
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Datum: | 6 Juli 2009 | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Nein | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | Expansion Deflection Nozzle Flow | ||||||||||||
Veranstaltungstitel: | 3RD EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS) | ||||||||||||
Veranstaltungsort: | Versailles/Paris, Frankreich | ||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||
Veranstaltungsbeginn: | 6 Juli 2009 | ||||||||||||
Veranstaltungsende: | 9 Juli 2009 | ||||||||||||
Veranstalter : | CNES/DLR | ||||||||||||
HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||
HGF - Programm: | Weltraum (alt) | ||||||||||||
HGF - Programmthema: | W RP - Raumtransport | ||||||||||||
DLR - Schwerpunkt: | Weltraum | ||||||||||||
DLR - Forschungsgebiet: | W RP - Raumtransport | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (alt) | ||||||||||||
Standort: | Lampoldshausen | ||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Technologie | ||||||||||||
Hinterlegt von: | Stark, Dr.-Ing. Ralf | ||||||||||||
Hinterlegt am: | 20 Jan 2010 08:29 | ||||||||||||
Letzte Änderung: | 24 Apr 2024 19:27 |
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