Design and Analysis of a Mechanism for the Chord and Camber Morphing of an Aircraft Wing

Date

2017-09-29

Author

Yaman, Yavuz

Metadata

Show full item record

Item Usage Stats

33
views

0
downloads

URI

https://hdl.handle.net/11511/85878

Conference Name

7th EASN International Conference on Innovation in European Aeronautics Research

Collections

Department of Aerospace Engineering, Conference / Seminar

Suggestions

OpenMETU
Core

Design and Analysis of a Novel Mechanism for the Morphing of Trailing Edge of an Aircraft Wing Şahin, Harun Levent; Yaman, Yavuz (2018-06-22) In this paper, design of a novel deployable scissor-structural mechanism (SSM) for active camber and chord morphing airfoil has been presented. The mechanism is created via combination of one four-bar linkage and various scissor-like elements (SLEs). The theory behind scissor-like elements and hierarchical design procedure are adequately explained. Following that design procedure, a scissor-structural mechanism is created in order to satisfy the desired airfoil shapes, which have different camber lines with...
Design and Evaluation of a Rotary Magnetorheological Fluid Device Featuring a Flexible Cartridge Taşcıoğlu, Yiğit; Topçu, Okan; Konukseven, Erhan İlhan (null; 2018-02-23)
Design and construction of a three dimensional milling dynamometer calibration and study of forces involved during milling. Study of tool life in milling. Razzaq, Abdul; Department of Mechanical Engineering (1970)
Design and development of a cylinder expansion test setup for determination of equation of state parameters of various explosives Topkaraoğlu, Emir; Ulaş, Abdullah; Department of Mechanical Engineering (2014) Explosives are energetic materials which are used for various military or civilian purposes. Several computer programs are used for predicting the behaviour of systems containing explosives. During modeling of various explosives in simulation software, Jones-Wilkins-Lee equation of state is widely used. However, the parameters used in JWL equation of state are not available for some of the explosives in open sources. A method called cylinder expansion test is used in order to determine these parameters. In ...
Design and construction of a shear force testing apparatus for bulk materials. Özalp, Y. Vasfi; Department of Mechanical Engineering (1984)

Citation Formats

Y. Yaman, “Design and Analysis of a Mechanism for the Chord and Camber Morphing of an Aircraft Wing,” 2017, p. 1, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/85878.