Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/4584
Title: Modal analysis of aerofoil cross-sectioned wing made of laninated composite and filled with foam
Other Titles: Köpükle doldurulmuş ve tabakalı kompozitten yapılmış aerofoil kesitli kanadın modal analizi
Authors: Yardımoğlu, Bülent
İskeçe, Barış
Keywords: Aircraft wings
Natural vibration
Modal analysis
ANSYS
Issue Date: Oct-2015
Publisher: Izmir Institute of Technology
Source: 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 Unpublished master's thesis, Izmir Institute of Technology, Izmir, Turkey
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.
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.
Description: Thesis (Master)--Izmir Institute of Technology, Mechanical Engineering, Izmir, 2015
Full text release delayed at author's request until 2018.11.23
Includes bibliographical references (leaves: 48-49)
Text in English; Abstract: Turkish and English
x, 49 leaves
URI: http://hdl.handle.net/11147/4584
Appears in Collections:Master Degree / Yüksek Lisans Tezleri

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