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A multiphasic continuum mechanical model for design investigations of an effusion-cooled rocket thrust chamber /

Zugl.: Stuttgart, University, Diss., 2005.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/315002752
Date January 2005
CreatorsGhadiani, Saeed Reza,
PublisherKöln : Deutsches Zentrum für Luft- und Raumfahrt e. V.,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
SourceKostenfrei

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