Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Büyük Oranda Şekil Değiştirebilen Kontrol Yüzeylerinin Yapısal Özelliklerinin Değerlendirilmesi
Date
2013-11-29
Author
Harun, Tıraş
İlhan Ozan, Tunçöz
Gürses, Ercan
Şahin, Melin
Özgen, Serkan
Yaman, Yavuz
Metadata
Show full item record
Item Usage Stats
238
views
0
downloads
Cite This
In this work the excitation forces, which are necessary for the required displacements of morphing control surfaces of an UAV, are studied. The work has been conducted within the context of an EU FP7 project ‘CHANGE, Combined morpHing Assessment software usiNG flight Envelope data and mission based morphing prototype wing development’ (CHANGE, 2012). The possible control surfaces of the wing were generated using CATIA V5-6R2012 software. Finite element analysis of the control surfaces was conducted by ANSYS 14.0 package program.
Subject Keywords
Morphing
,
Control Surfaces
,
Finite Element Analysis
URI
https://hdl.handle.net/11511/78741
http://ae.metu.edu.tr/~yyaman/Publications/National/64.pdf
Conference Name
II. Ulusal Havacılık Teknolojisi ve Uygulamaları Kongresi, 2013
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
Static and dynamic aeroelastic analysis of a very light Aircraft
Demirer, Halime Gül; Kayran, Altan; Department of Aerospace Engineering (2021-9-10)
Aircraft design processes need to ensure that the aircraft is aeroelastically stable within its operational envelope. This thesis presents an overview of the static aeroelastic, flutter and gust response analysis of a very light aircraft. MSC.FlightLoads and MSC.Nastran are used for aeroelastic modeling and analysis. The methods to be used in the aeroelastic analysis of the VLA are tested on the AGARD 445.6 wing, and the results are in good agreement with the literature. Aeroelastic model corrections such a...
Büyük Oranda Şekil Değiştirebilen Bir Hibrid Firar Kenarı Kontrol Yüzeyinin Tasarımı ve Analizleri
İlhan Ozan, Tunçöz; Yosheph, Yang; Gürses, Ercan; Şahin, Melin; Özgen, Serkan; Yaman, Yavuz (2015-10-23)
It is envisioned that the fully morphing wings and/ or control surfaces, as they can increase the aerodynamic efficiency of the airplanes in every phases of the flight, could play significant role in the reduction of pollution in environment and also make airplanes always fuel efficient. In this study, the design and analyses of a fully morphing trailing edge control surface, which is developed within the scope of CHANGE Project, are presented. The Project was a 7th Framework Programme Project of European C...
Büyük Oranda Şekil Değiştirebilen Kanat Yüzeylerinin Aerodinamik Yükler Altında Davranışları
Arslan, Pınar; Uğur, Kalkan; Yosheph, Yang; Özgen, Serkan; Şahin, Melin; Gürses, Ercan; Yaman, Yavuz (2013-11-29)
In this study, a morphing wing’s structural properties are examined under the aerodynamic loads. This study is conducted within the scope of the 7th Framework Programme of the European Comission project ‘CHANGE, Combined morpHing Assesment software usiNG flight Envelope data and mission based morphing prototype wing development’ (CHANGE, 2012). For the Computational Fluid Dynamics (CFD) analysis ANSYS Fluent® 14.0 is used as a package program. For the Structural analysis, ANSYS Static Struc...
Büyük Oranda Şekil Değiştirebilen Kanat Yüzeylerinin Aerodinamik Yükler Altındaki Davranışları
Arslan, Pınar; Kalkan, Uğur; Tıraş, Harun; Tunçöz, İlhan Ozan; Yang, Yosheph; Gürses, Ercan; Şahin, Melin; Özgen, Serkan; Yaman, Yavuz (2013-11-30)
In this study, a morphing wing’s structural properties are examined under the aerodynamic loads. This study is conducted within the scope of the 7th Framework Programme of the European Comission project ‘CHANGE, Combined morpHing Assesment software usiNG flight Envelope data and mission based morphing prototype wing development’ (CHANGE, 2012). For the Computational Fluid Dynamics (CFD) analysis ANSYS Fluent® 14.0 is used as a package program. For the Structural analysis, ANSYS Static Structural® 14.0 packa...
Measurement of nonuniform magnetized argon plasma discharge parameters
Dağtekin, Ebru; Bilikmen, Kadri Sinan; Department of Physics (2006)
Effects of a magnetic field on the double-probe technique are studied experimentally by means of symmetric floating computer controlled fast double probes in low and intermediate pressure plasmas. In addition, the effects of the magnetic field on the electron temperature, electron density, and electric field have been investigated. As it is expected, when there is no magnetic field, properties of the discharge plasma are best described by Langmuir theory. Whereas, when there’s a magnetic field of sufficient...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
T. Harun, T. İlhan Ozan, E. Gürses, M. Şahin, S. Özgen, and Y. Yaman, “Büyük Oranda Şekil Değiştirebilen Kontrol Yüzeylerinin Yapısal Özelliklerinin Değerlendirilmesi,” presented at the II. Ulusal Havacılık Teknolojisi ve Uygulamaları Kongresi, 2013, İzmir, Türkiye, 2013, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/78741.
