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Büyük Oranda Şekil Değiştirebilen Kanatların Aerodinamik ve Yapısal Tasarımı
Date
2012-06-20
Author
Ünlüsoy, Levent
Körpe, Durmuş Sinan
Şahin, Melin
Özgen, Serkan
Yaman, Yavuz
Metadata
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Bu çalışmada, son yıllarda göreve uyumlu havacılık yapıları ve malzemelerinin üretim teknolojilerindeki gelişmelerle ortaya çıkan ve uçakların havadayken farklı görev evrelerinde (dalış, tırmanma, düz uçuş, dönüş, bekleme, vb.) en iyi performansı verebilecek şekilde uçabilmesini sağlayabilecek, büyük oranda şekil değiştirebilen (fully morphing) kanatların aerodinamik ve yapısal tasarım süreci ve en iyileştirilmesi üzerine izlenen yol anlatılmıştır.
Subject Keywords
Morphing wings
,
Wing design
,
Multidisciplinary optimization
,
Şekil değiştirebilen kanatlar
,
Kanat tasarımı
,
Çoklu disiplinlerde en iyileştirilme
URI
https://hdl.handle.net/11511/75653
Conference Name
SAVUNMA TEKNOLOJİLERİ KONGRESİ, SAVTEK 2012
Collections
Department of Aerospace Engineering, Conference / Seminar
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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...
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 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...
Design and analysis of a hybrid trailing edge control surface of a fully morphing unmanned aerial vehicle wing
Tunçöz, İlhan Ozan; Yaman, Yavuz; Department of Aerospace Engineering (2015)
In this thesis, the design and analysis of a hybrid trailing edge control surface of a fully morphing unmanned aerial vehicle wing having the ability to perform both camber and decamber morphings were conducted. The design of the control surface was done by CATIA V5-6R2012 package program. Two distinct designs, so-called open cell and closed cell designs were initially analyzed via Finite Element Method by using the commercial software ANSYS Workbench v14.0 in in-vacuo condition. Several trade-off studies i...
Structural design and analysis of the mission adaptive wings of an unmanned aerial vehicle
Ünlüsoy, Levent; Yaman, Yavuz; Department of Aerospace Engineering (2010)
In this study, the structural design and analysis of a wing having mission-adaptive control surfaces were conducted. The wing structure was designed in order to withstand a maximum aerodynamic loading of 5 g due to maneuver. The structural model of the wing was developed by using MSC/PATRAN package program and that structural model was analyzed by using MSC/NASTRAN package program. The designed wing was then manufactured by Turkish Aerospace Industries Inc. (TUSAŞ-TAI). The finite element analysis results w...
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L. Ünlüsoy, D. S. Körpe, M. Şahin, S. Özgen, and Y. Yaman, “Büyük Oranda Şekil Değiştirebilen Kanatların Aerodinamik ve Yapısal Tasarımı,” presented at the SAVUNMA TEKNOLOJİLERİ KONGRESİ, SAVTEK 2012, 20-22 Haziran 2012, ODTÜ, Ankara, 2012, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/75653.
