A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets (Englisch)
- Neue Suche nach: Di Martino, Giuseppe D.
- Neue Suche nach: Malgieri, Paolo
- Neue Suche nach: Carmicino, Carmine
- Neue Suche nach: Savino, Raffaele
- Neue Suche nach: Di Martino, Giuseppe D.
- Neue Suche nach: Malgieri, Paolo
- Neue Suche nach: Carmicino, Carmine
- Neue Suche nach: Savino, Raffaele
In:
Acta astronautica
;
129
;
8-21
;
2016
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ISSN:
- Aufsatz (Zeitschrift) / Print
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Titel:A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets
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Beteiligte:Di Martino, Giuseppe D. ( Autor:in ) / Malgieri, Paolo ( Autor:in ) / Carmicino, Carmine ( Autor:in ) / Savino, Raffaele ( Autor:in )
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Erschienen in:Acta astronautica ; 129 ; 8-21
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Verlag:
- Neue Suche nach: Elsevier Science B.V., Amsterdam.
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Erscheinungsdatum:01.01.2016
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Format / Umfang:14 pages
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ISSN:
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Medientyp:Aufsatz (Zeitschrift)
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Format:Print
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Sprache:Englisch
- Neue Suche nach: 629.405
- Weitere Informationen zu Dewey Decimal Classification
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Klassifikation:
DDC: 629.405 -
Datenquelle:
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