Shin, H. und Oschwald, M. und Micci, M.M. und Yoon, W. (2005) Influence of Thermodynamic State on Nanojet Break-up. Nanotechnology, 16, Seiten 2838-2845.
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Kurzfassung
Using a non-equilibrium molecular dynamics, argon nanojet injection was simulated under vacuum condition. A series of simulations with different shapes of solid platinum injectors were conducted. Observed droplet sizes and jet breakup characteristics resemble the Rayleigh breakup theory. However, the different injector shapes do not cause the remarkable change in nanojet breakup behaviour. The liquid temperature inside the injector is the controlling factor to determine the subsequent breakup characteristics. Higher liquid temperature is preferred for the faster nanojet breakup with the shorter breakup length.
elib-URL des Eintrags: | https://elib.dlr.de/53416/ | ||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||
Titel: | Influence of Thermodynamic State on Nanojet Break-up | ||||||||||||||||||||
Autoren: |
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Datum: | 2005 | ||||||||||||||||||||
Erschienen in: | Nanotechnology | ||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
Band: | 16 | ||||||||||||||||||||
Seitenbereich: | Seiten 2838-2845 | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | molecular dynamics simulation | ||||||||||||||||||||
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: | Oschwald, Dr.rer.nat. Michael | ||||||||||||||||||||
Hinterlegt am: | 26 Feb 2008 | ||||||||||||||||||||
Letzte Änderung: | 31 Jul 2019 19:21 |
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