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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 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...
Büyük Oranda Şekil Değiştirebilen Bir Hibrid Firar Kenarı Kontrol Yüzeyinin Tasarımı ve Analizleri
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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 of a traverse system for the characterization of a large-scale wind tunnel
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This study presents the design and simulations of a traverse system and preliminary characterization measurements of the RÜZGEM large-scale wind tunnel. In the first phase of the study, the traverse system was simulated aerodynamically using computational fluid dynamics (CFD) tools. The effects of the rectangular, whole profile and partial profile traverse mechanisms on the measurements were examined. The probe lengths were studied in detail to determine the most suitable length. According to the simulation...
Aero-structural analysis of the morphing trailing edge control surface of a fully morphing unmanned aerial vehicle wing
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This thesis investigates the aero-structural analysis of the morphing trailing edge control surface of a fully morphing unmanned aerial vehicle wing for some camber morphing missions. Designed control surface was structurally analyzed with Finite Element Method using ANSYS Workbench v14.0 Static Structural module. Open Cell, Closed Cell designs with some material and thickness changes were studied in order to find the optimum design in terms of minimum weight and structural relevance. Analyses were both per...
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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.