Klein, Sebastian und Traudt, Tobias und Deeken, Jan C. (2025) Cryogenic Pressure Surge Data Set: PS-LN2-Set1. [sonstige Veröffentlichung]
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Offizielle URL: https://zenodo.org/records/15526459
Kurzfassung
Cryogenic fluid hammer experiments have been performed at the Fluid Transient Fest Facility (FTTF) at the Institute of Space Propulsion of the German Aerospace Center (DLR) in Lampoldshausen. A pressure surge is created by using a fast closing valve to stop a stationary flow of liquid nitrogen in a pipeline. The pressure wave is then travelling back and forth between the valve and a reservoir upstream of the pipe. Due to the high amplitude of this pressure wave, the pressure drops below the vapor pressure, causing cavitation near the valve. The dataset includes 9 test cases across a wide range of pressure and flow velocity. At maximum, a flow velocity of 13 m/s results in a pressure surge amplitude exceeding 100 bar. It also features high-frequency pressure sensors, providing detailed insights into the phenomenon.
elib-URL des Eintrags: | https://elib.dlr.de/214268/ | ||||||||||||||||
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Dokumentart: | sonstige Veröffentlichung | ||||||||||||||||
Titel: | Cryogenic Pressure Surge Data Set: PS-LN2-Set1 | ||||||||||||||||
Autoren: |
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Datum: | 22 Mai 2025 | ||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||
Open Access: | Nein | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | fluid hammer, cavitation, pressure surge, liquid nitrogen, rocket engine, feed line system, fluid transients | ||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Leitprojekt - Forschungsverbund Oberstufe | ||||||||||||||||
Standort: | Lampoldshausen | ||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Raketenantriebssysteme | ||||||||||||||||
Hinterlegt von: | Hanke, Michaela | ||||||||||||||||
Hinterlegt am: | 27 Jun 2025 11:39 | ||||||||||||||||
Letzte Änderung: | 27 Jun 2025 11:39 |
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