Modal analysis of aerofoil cross-sectioned wing made of laninated composite and filled with foam

İskeçe, Barış

Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/4584

Full metadata record

DC Field	Value	Language
dc.contributor.advisor	Yardımoğlu, Bülent	en_US
dc.contributor.author	İskeçe, Barış	-
dc.date.accessioned	2016-04-29T13:40:35Z	-
dc.date.available	2016-04-29T13:40:35Z	-
dc.date.issued	2015-10	-
dc.identifier.citation	İskeçe, B. (2015). Modal analysis of aerofoil cross-sectioned wing made of laninated composite and filled with foam. Unpublished master's thesis, Izmir Institute of Technology, Izmir, Turkey	en_US
dc.identifier.uri	http://hdl.handle.net/11147/4584	-
dc.description	Thesis (Master)--Izmir Institute of Technology, Mechanical Engineering, Izmir, 2015	en_US
dc.description	Full text release delayed at author's request until 2018.11.23	en_US
dc.description	Includes bibliographical references (leaves: 48-49)	en_US
dc.description	Text in English; Abstract: Turkish and English	en_US
dc.description	x, 49 leaves	en_US
dc.description.abstract	Modal analysis of aerofoil cross-sectioned wing made of laminated composite and filled with foam is studied by Finite Element Method with the help of ANSYS which is very powerful and well proven software all around the world. The effects of ratio of overhangs to mid-span and length of the thickened parts on natural frequencies are investigated by finite element models developed in ANSYS and the model is verified by theoretical results available in the literature.	en_US
dc.description.abstract	Köpükle doldurulmuş ve tabakalı kompozitten yapılmış aerofoil kesitli kanadın modal analizi, Dünya’da iyi ispatlanmış ve güçlü bir sonlu eleman yazılımı olan ANSYS’in yardımı ile çalışılmıştır. Çıkıntının açıklığa oranının ve takviyelenmiş kısımların uzunluklarının doğal frekanslara etkileri ANSYS de geliştirilen sonlu eleman modelleri ile araştırılmıştır ve model kaynaklarda mevcut sonuçlar ile karşılaştırılarak doğrulanmıştır.	en_US
dc.language.iso	en	en_US
dc.publisher	Izmir Institute of Technology	en_US
dc.rights	info:eu-repo/semantics/openAccess	en_US
dc.subject	Aircraft wings	en_US
dc.subject	Natural vibration	en_US
dc.subject	Modal analysis	en_US
dc.subject	ANSYS	en_US
dc.title	Modal analysis of aerofoil cross-sectioned wing made of laninated composite and filled with foam	en_US
dc.title.alternative	Köpükle doldurulmuş ve tabakalı kompozitten yapılmış aerofoil kesitli kanadın modal analizi	en_US
dc.type	Master Thesis	en_US
dc.institutionauthor	İskeçe, Barış	-
dc.department	Thesis (Master)--İzmir Institute of Technology, Mechanical Engineering	en_US
dc.relation.publicationcategory	Tez	en_US
item.openairecristype	http://purl.org/coar/resource_type/c_18cf	-
item.cerifentitytype	Publications	-
item.fulltext	With Fulltext	-
item.languageiso639-1	en	-
item.grantfulltext	open	-
item.openairetype	Master Thesis	-
Appears in Collections:	Master Degree / Yüksek Lisans Tezleri