Applying Finite Element Method to Buckling Analyses of Composite Helicopter Structures



Title:	Applying Finite Element Method to Buckling Analyses of Composite Helicopter Structures Elementtimenetelmän soveltaminen komposiittisten helikopterirakenteiden lommahdusanalyyseihin
Author(s):	Heikkilä, Jarkko
Date:	2002
Language:	en
Pages:	x + 86 s. + liitt.
Department:	Konetekniikan osasto
Major/Subject:	Lentotekniikka
Supervising professor(s):	Saarela, Olli
Thesis advisor(s):	Majamäki, Jyrki
Keywords:	buckling, lommahtaminen, composite, komposiitti, FEM, epälineaarinen, non-linear, lineaarinen, linear, testi, validation, pakkosiirtymä, test, forced displacement
Location:	Archive
	OEVS yes
Digitized thesis:	ask
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Permanent link to this item: http://urn.fi/URN:NBN:fi:aalto-2020120448388 Email this Export to RefWorks QR Code Print BibTex Tweet