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 Gürses, Ercan; Yang, Yosheph; Arslan, Pinar; Kalkan, Ugur; Tıraş, Harun; Şahin, Melin; Özgen, Serkan; Yaman, Yavuz (2017-05-01) In this article, the design and analysis of a hybrid trailing edge control surface of an unmanned aerial vehicle are presented. The structural design was performed to increase and decrease the camber of the control surface to match selected airfoil profiles. The design was first analyzed with the help of finite element method to assess the morphing capability. The morphed control surface was then analyzed aerodynamically and comparisons with the original target profiles were made. According to the aerodynam...
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Citation Formats

P. Arslan et al., “A hybrid trailing edge control surface concept,” 2014, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/82204.