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Flow Processes in Rocket Engine Nozzles with Focus on Flow Separation and Side-Loads
KTH, Superseded Departments, Mechanics.
2002 (English)Licentiate thesis, comprehensive summary (Other scientific)
Place, publisher, year, edition, pages
Stockholm: Mekanik , 2002. , 122 p.
Series
Trita-MEK, ISSN 0348-467X ; 2002:09
Keyword [en]
turbulent, boundary layer, shock wave, interaction, intermittent, overexpanded, rocket nozzle, flow separation, side-load, models, criteria, prediction, review
Identifiers
URN: urn:nbn:se:kth:diva-1452ISBN: OAI: oai:DiVA.org:kth-1452DiVA: diva2:7328
Note
NR 20140805Available from: 2002-06-25 Created: 2002-06-25Bibliographically approved

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8b9c914404a906dc3a2e46e583f8b186351794cf4bc015d9fcef9e7aa35660b53069907f
Type fulltextMimetype application/pdf

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CiteExportLink to record
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Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
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More styles
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  • de-DE
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