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A hybrid trailing edge control surface concept
Date
2014-05-25
Author
Arslan, Pınar
Uğur, Kalkan
Harun, Tıraş
İlhan Ozan, Tunçöz
Yosheph, Yang
Gürses, Ercan
Şahin, Melin
Özgen, Serkan
Yaman, Yavuz
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This study presents the design and analysis of a novel hybrid trailing edge control surface that is capable to perform both camber and decamber morphing. The design was conducted with CATIA V5-6R2012 package program. Structural analyses were performed with Finite Element Method by using ANSYS® Workbench™ v14.0 package program both in in-vacuo condition and under aerodynamic loading. The aerodynamic loads were calculated by Computational Fluid Dynamics analyses. The required aerodynamic mesh was generated by Pointwise® V17.2 R2 package program, and SU2 (Stanford University Unstructured) V3.2.1 open source software was used as flow solver. The results prove that the designed control surface is capable of performing both camber and decamber morphing both in in-vacuo condition and under aerodynamic loading.
Subject Keywords
Morphing Control Surface
,
Finite element analysis
,
Computational fluid dynamics
,
Aerodynamic analysis
,
Structural design
URI
https://hdl.handle.net/11511/82204
https://www.researchgate.net/publication/280313432_A_Hybrid_Trailing_Edge_Control_Surface_Capable_of_Camber_and_Decamber_Morphing
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Department of Aerospace Engineering, Conference / Seminar
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A Hybrid Trailing Edge Control Surface Capable of Camber and Decamber Morphing
İlhan Ozan, Tunçöz; Yosheph, Yang; Gürses, Ercan; Şahin, Melin; Özgen, Serkan; Yaman, Yavuz (2015-06-03)
This study presents the design and analysis of a novel hybrid trailing edge control surface that is capable to perform both camber and decamber morphing. The design was conducted with CATIA V5-6R2012 package program. Structural analyses were performed with Finite Element Method by using ANSYS® Workbench™ v14.0 package program both in in-vacuo condition and under aerodynamic loading. The aerodynamic loads were calculated by Computational Fluid Dynamics analyses. The required aerodynamic mesh was generated by...
Structural and aerodynamic analyses of a hybrid trailing edge control surface of a fully morphing wing
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Design and analysis of a hybrid trailing edge control surface of a fully morphing unmanned aerial vehicle wing
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Structural analysis of morphing control surfaces
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In this thesis, design and analysis of a hybrid trailing edge control surface is performed. Only camber motion and twisting motion of the trailing edge control surface are considered. There are four control surface configurations that are analyzed. For the first configuration, servo actuators actuating the control surface are inside the control surface volume and control surface is without pre-twist. For the second case, the control surface is pre-twisted and actuators are inside the control surface volume....
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P. Arslan et al., “A hybrid trailing edge control surface concept,” 2014, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/82204.
