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Rocket Engine System Analysis : Vinci Engine Turbines Analysis, Volvo Aero Corp.

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).

Identiferoai:union.ndltd.org:UPSALLA1/oai:DiVA.org:liu-17766
Date January 2008
CreatorsRomanov, Artyom
PublisherLinköpings universitet, Mekanisk värmeteori och strömningslära, Linköpings universitet, Linköpings universitet, Institutionen för ekonomisk och industriell utveckling
Source SetsDiVA Archive at Upsalla University
LanguageEnglish
Detected LanguageEnglish
TypeStudent thesis, info:eu-repo/semantics/masterThesis, text
Formatapplication/pdf
Rightsinfo:eu-repo/semantics/openAccess

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