Modal analysis of aerofoil cross-sectioned wing made of laninated composite and filled with foam
by
İskeçe, Barış, author.
Title
:
Modal analysis of aerofoil cross-sectioned wing made of laninated composite and filled with foam
Author
:
İskeçe, Barış, author.
Personal Author
:
İskeçe, Barış, author.
Physical Description
:
x, 49 leaves.: + 1 computer laser optical disc.
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.
Subject Term
:
Airplanes -- Wings -- Vibration.
Airplanes -- Wings -- Design.
Aerofoils -- Testing.
Modal analysis.
Added Author
:
Yardımoğlu, Bülent
Added Corporate Author
:
İzmir Institute of Technology. Mechanical Engineering.
Added Uniform Title
:
Thesis (Master)--İzmir Institute of Technology:Mechanical Engineering.
İzmir Institute of Technology: Mechanical Engineering--Thesis (Master).
Electronic Access
:
| Library | Material Type | Item Barcode | Shelf Number | Status |
|---|
| IYTE Library | Thesis | T001447 | TL672 .I81 2015 | Tez Koleksiyonu |
| IYTE Library | Supplementary CD-ROM | ROM2537 | TL672 .I81 2015 | Tez Koleksiyonu |