Modal analysis of aerofoil cross-sectioned wing made of laninated composite and filled with foam
tarafından
 
İskeçe, Barış, author.

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

Yazar
: 
İskeçe, Barış, author.

Yazar Ek Girişi
: 
İskeçe, Barış, author.

Fiziksel Tanımlama
: 
x, 49 leaves.: + 1 computer laser optical disc.

Özet
: 
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.

Konu Başlığı
: 
Airplanes -- Wings -- Vibration.
 
Airplanes -- Wings -- Design.
 
Aerofoils -- Testing.
 
Modal analysis.

Yazar Ek Girişi
: 
Yardımoğlu, Bülent

Tüzel Kişi Ek Girişi
: 
İzmir Institute of Technology. Mechanical Engineering.

Tek Biçim Eser Adı
: 
Thesis (Master)--İzmir Institute of Technology:Mechanical Engineering.
 
İzmir Institute of Technology: Mechanical Engineering--Thesis (Master).

Elektronik Erişim
: 
Access to Electronic Versiyon.


LibraryMateryal TürüDemirbaş NumarasıYer NumarasıDurumu/İade Tarihi
IYTE LibraryTezT001447TL672 .I81 2015Tez Koleksiyonu