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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
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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
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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.
