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
Department
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Lentotekniikka
Mcode
Kul-34
Degree programme
Language
en
Pages
x + 86 s. + liitt.
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Description
Supervisor
Saarela, OlliThesis advisor
Majamäki, JyrkiKeywords
buckling, lommahtaminen, composite, komposiitti, FEM, epälineaarinen, non-linear, lineaarinen, linear, testi, validation, pakkosiirtymä, test, forced displacement