Liang, Jianghan und Cai, Xiaodong und Lin, Zhiyong und Deiterding, Ralf (2014) Effects of a hot jet on detonation initiation and propagation in supersonic combustible mixtures. Acta Astronautica, 105 (1), Seiten 265-277. Elsevier. doi: 10.1016/j.actaastro.2014.08.019. ISSN 0094-5765.
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Offizielle URL: http://dx.doi.org/10.1016/j.actaastro.2014.08.019
Kurzfassung
The effects of a hot jet on detonation initiation and propagation in supersonic combustible mixtures has been studied with two-dimensional numerical simulations with the open-source program AMROC that uses a block-structured adaptive mesh refinement method. Results indicate that the hot jet could ignite the detonation effectively in supersonic combustible mixtures like a pneumatic ramp. After the realization of the detonation initiation, the hot jet can still play an important role on the detonation propagation during its continuous ejection. For a hot jet with certain diameter, it can result in an overdriven detonation with almost constant overdrive degree. After the shutdown of the hot jet, the stable CJ detonation combustion was realized finally in the supersonic combustible mixtures. With the re-ejection of the hot jet, the failed detonation could be reinitiated quickly. Through the control of the re-ejection of the hot jet, it plays a key role not only in the initiation process, but also in the subsequent continuous detonation combustion period.
elib-URL des Eintrags: | https://elib.dlr.de/95320/ | ||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||
Zusätzliche Informationen: | Published online: 03. Sept. 2014 | ||||||||||||||||||||
Titel: | Effects of a hot jet on detonation initiation and propagation in supersonic combustible mixtures | ||||||||||||||||||||
Autoren: |
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Datum: | 2014 | ||||||||||||||||||||
Erschienen in: | Acta Astronautica | ||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||
Band: | 105 | ||||||||||||||||||||
DOI: | 10.1016/j.actaastro.2014.08.019 | ||||||||||||||||||||
Seitenbereich: | Seiten 265-277 | ||||||||||||||||||||
Verlag: | Elsevier | ||||||||||||||||||||
Name der Reihe: | ScienceDirect | ||||||||||||||||||||
ISSN: | 0094-5765 | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | adaptive mesh refinement, simulation, detonation | ||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Systeme und Kabine (alt) | ||||||||||||||||||||
Standort: | Göttingen | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Fluidsysteme | ||||||||||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||
Hinterlegt am: | 25 Feb 2015 15:25 | ||||||||||||||||||||
Letzte Änderung: | 10 Jan 2019 15:39 |
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