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Rocket Engine System Analysis: Vinci Engine Turbines Analysis, Volvo Aero Corp.
Linköping University, Department of Management and Engineering, Applied Thermodynamics and Fluid Mechanics . Linköping University. Linköping University, Department of Management and Engineering.
2008 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

Major part of the current work describes the development of the update methodology for onedimensional code (TML) currently used at Volvo Aero Corporation during turbine design process. The methodology is then applied and tried out in a general engine analysis (GESTPAN).

Place, publisher, year, edition, pages
2008. , 108 p.
Keyword [en]
volvo aero vinci rocket rotor turbine system analysis space ariane 5
Identifiers
URN: urn:nbn:se:liu:diva-17766ISRN: LIU‐IEI‐TEK‐A--08/00493—SEOAI: oai:DiVA.org:liu-17766DiVA: diva2:211749
Presentation
2008-12-02, IKP2, Linköpings universitet, Campus Valla, Linköping, 10:00 (Swedish)
Uppsok
teknik
Supervisors
Examiners
Available from: 2009-04-20 Created: 2009-04-17 Last updated: 2009-04-20Bibliographically approved

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Applied Thermodynamics and Fluid Mechanics Linköping UniversityDepartment of Management and Engineering

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CiteExportLink to record
Permanent link

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Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • oxford
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf