Génin, Chloé und Stark, Ralf (2011) Hot flow testing of dual bell nozzles. 49th Aerospace Science Meeting, 2011-01-04 - 2011-01-07, Orlando, Florida.
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Kurzfassung
The dual bell nozzle offers a simple and efficient altitude adaption through its contour inflection, which insures a symmetrical and controlled separation at sea level and a large area ratio at high altitude. The conditions for the flow transition from one operating mode to the other have been intensively investigated in cold flow conditions. A test campaign has been conducted on two dual bell nozzle geometries to verify the theoretical prediction criterion and to investigate the influence of the temperature variations. Therefore, a thin walled axisymmetric and a planar nozzle were designed and tested under hot flow conditions. Wall temperature measurements have been made using both thermocouples and thermal imaging. The region of the contour inflection was of particular interest for the evaluation of thermal behavior in the nozzle wall.
elib-URL des Eintrags: | https://elib.dlr.de/68377/ | ||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||
Zusätzliche Informationen: | AIAA-2011-0387 | ||||||||||||
Titel: | Hot flow testing of dual bell nozzles | ||||||||||||
Autoren: |
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Datum: | 2011 | ||||||||||||
Referierte Publikation: | Ja | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Nein | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | expermental study, nozzle flow, dual bell | ||||||||||||
Veranstaltungstitel: | 49th Aerospace Science Meeting | ||||||||||||
Veranstaltungsort: | Orlando, Florida | ||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||
Veranstaltungsbeginn: | 4 Januar 2011 | ||||||||||||
Veranstaltungsende: | 7 Januar 2011 | ||||||||||||
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: | Nürnberger-Genin, Chloe | ||||||||||||
Hinterlegt am: | 14 Jan 2011 09:49 | ||||||||||||
Letzte Änderung: | 24 Apr 2024 19:33 |
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