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Sizing and Balance Module Development for Aircraft Conceptual Design

This thesis work was done in order to improve the capabilities in a preliminary aircraft analysis program, DIBA, at Saab Aerosystems. The areas that this was done are in the sizing and balance. One sizing tool was developed in order to make a performance analysis with the DIBA generated geometry and customer and/or regulation based criteria. A balance diagram, a neutral point estimation function, a landing gear plot and a trim program was created in order to extend the weight and balance analysis. Results show that various aircraft both military and civil can be analyzed with good comparison to other analysis and reality. For example EXCEL implemented analysis and graphs over real aircrafts shown in the report.

Identiferoai:union.ndltd.org:UPSALLA1/oai:DiVA.org:liu-9999
Date January 2007
CreatorsPeterson, Gustav
PublisherLinköpings universitet, Institutionen för ekonomisk och industriell utveckling, Institutionen för ekonomisk och industriell utveckling
Source SetsDiVA Archive at Upsalla University
LanguageEnglish
Detected LanguageEnglish
TypeStudent thesis, info:eu-repo/semantics/bachelorThesis, text
Formatapplication/pdf
Rightsinfo:eu-repo/semantics/openAccess

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