Project of designing, building and analysis of a metallic stringer for aerospace applications. Loading and verification until range of elastic instability.
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hdl:2117/177591
Document typeBachelor thesis
Date2014-06
Rights accessRestricted access - author's decision
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Abstract
The research in light weight structures is a crucial characteristic of the aerospace industry. The stringers with web buckling capability appeared as a result of this constant research. In this project, it is analyzed analytically, experimentally and numerically this kind of optimized structures to finish with the designing and building of an improved design which will serve as the basis for a laboratory practice in the subject of aerospace structures
SubjectsLarge space structures (Astronautics)--Design and construction, Grans estructures espacials (Astronàutica) -- Disseny i construcció
DegreeGRAU EN ENGINYERIA EN TECNOLOGIES AEROESPACIALS (Pla 2010)
Files | Description | Size | Format | View |
---|---|---|---|---|
annex I.pdf![]() | 3,509Mb | Restricted access | ||
Annex II_2.pdf![]() | 3,033Mb | Restricted access | ||
Annex III_2.pdf![]() | 1,749Mb | Restricted access | ||
Report_7.pdf![]() | 820,9Kb | Restricted access | ||
Budget_9.pdf![]() | 488,7Kb | Restricted access | ||
Technical Sheet.pdf![]() | 367,8Kb | Restricted access |