Büyük Oranda Şekil Değiştirebilen Kanatlar ve Kontrol Yüzeylerine Sahip Geleceğin Hava Taşıtları

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2017-04-07

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Yaman, Yavuz

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https://hdl.handle.net/11511/77184

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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 Kanatlar İçin Kambur Değişimi Sağlayan Bir Mekanizmanın Tasarımı Şahin, Harun Levent; Yaman, Yavuz (null; 2016-09-30)
Büyük Oranda Şekil Değiştirebilen Kanat Kontrol Yüzeylerinin Uçuştaki Etkileri Yaman, Yavuz; Özgen, Serkan; Şahin, Melin; Gürses, Ercan (null; 2012-12-20)
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...

Citation Formats

Y. Yaman, “Büyük Oranda Şekil Değiştirebilen Kanatlar ve Kontrol Yüzeylerine Sahip Geleceğin Hava Taşıtları,” 2017, Accessed: 00, 2021. [Online]. Available: www.sares.org.