Şekil Değiştiren Uçaklar ve Gelecek

Date

2015-02-26

Author

Yaman, Yavuz

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https://hdl.handle.net/11511/78563

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Şekil Değiştiren Uçaklar Havacılıkta Yeni Bir Devrim Yaratabilir mi Özgen, Serkan; Şahin, Melin; Yaman, Yavuz; Bayram, Göknur; Yılmaz, Ayşen (2008-01-01)
Şekil Değiştiren Uçaklar Havacılıkta Yeni Bir Devrim Yaratabilir mi? Yaman, Yavuz; Özgen, Serkan; Bayram, Göknur; Uludağ, Yusuf; Yılmaz, Ayşen (2008-02-01)
Şekil Değiştiren Kanatlara ve Kontrol Yüzeylerine Sahip Uçaklar Yaman, Yavuz (null; 2015-04-21)
Design, Modelling and Analysis of Morphing Airfoils Köksal, Buğra; Şahin, Melin; Uzol, Oğuz; Department of Aerospace Engineering (2023-1) This study presents the design, finite element (FE) modeling and analysis of a morphing airfoil using pressure-actuated cell structures. It is aimed that the selected baseline airfoil should be capable of changing its profile to morph into a target airfoil profile. To achieve this goal, first, a NACA 0012 airfoil with a 500 mm chord and 8 mm x 8 mm outer cross-section is obtained in Altair® HyperWorks environment as a baseline airfoil. Following this, the cell actuators responsible for morphing are designed...
Experimental investigation of morphing wing aerodynamics by force measurements and particle image velocimetry Özçakmak, Özge Sinem; Özgen, Serkan; Department of Aerospace Engineering (2015) Recently, new developments in on manufacturing technologies, aircraft materials, sensors, actuators, and other mechanisms raised the interest in morphing wings. Instead of conventional wings, which are optimized only for one flight condition, morphing wings can adapt themselves for different missions, mission segments and associated flight conditions. The focus of this thesis is the experimental analysis of a morphing wing, the planform and airfoil shapes that were made available from a separate numerical s...

Citation Formats

Y. Yaman, “Şekil Değiştiren Uçaklar ve Gelecek,” 2015, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/78563.