Applying Finite Element Method to Buckling Analyses of Composite Helicopter Structures

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Helsinki University of Technology | Diplomityö
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Date
2002
Major/Subject
Lentotekniikka
Mcode
Kul-34
Degree programme
Language
en
Pages
x + 86 s. + liitt.
Series
Description
Supervisor
Saarela, Olli
Thesis advisor
Majamäki, Jyrki
Keywords
buckling, lommahtaminen, composite, komposiitti, FEM, epälineaarinen, non-linear, lineaarinen, linear, testi, validation, pakkosiirtymä, test, forced displacement
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