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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: | İskeçe, Barış | Advisors: | Yardımoğlu, Bülent | Keywords: | Aircraft wings Natural vibration Modal analysis ANSYS |
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 Unpublished master's thesis, Izmir Institute of Technology, Izmir, Turkey | Abstract: | Modal analysis of aerofoil cross-sectioned wing made of laminated composite and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 |
Files in This Item:
File | Description | Size | Format | |
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T001447.pdf | MasterThesis | 716.67 kB | Adobe PDF | View/Open |
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