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Open Access

Deployment of SMP Miura-ori sheet and its application: Aerodynamic drag and RCS reduction

Ji ZHANGa,bChangguo WANGa,bLamei ZHANGc( )
National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China
Center for Composite Materials and Structures, Harbin Institute of Technology, Harbin 150001, China
Department of Information Engineering, Harbin Institute of Technology, Harbin 150001, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Origami, such as Miura-ori, is the art of folding two-dimensional materials into complex, elaborate, and multifunctional three-dimensional objects. In this paper, SMP MO sheet are prepared, and the accuracy of deployable process is verified by experiments. The folding and deployable process of SMP MO sheet is divided into 4 stages, and each stage is described in detail. The stiffness of smart deployable stage is characterized by an exponential decline at the beginning and a gradual decrease to 0, and this is similar to the theoretical shear equivalent modulus in the Y direction. The effects of various parameters on strain and stress are also explored. The purpose of studying these mechanical characteristics is to provide driving force reference in application; In terms of application, the flow field and electromagnetic characteristics of MO sheet in different directions are studied. The aerodynamic drag and RCS reduction of MO unit cell and graded MO sheet during the deployable process are evaluated. When the dihedral fold angle is about 45°, the RCS reduction and drag reduction characteristics of MO sheet are relatively optimal, which is most beneficial to morphing aircraft.

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Chinese Journal of Aeronautics
Pages 121-131

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Cite this article:
ZHANG J, WANG C, ZHANG L. Deployment of SMP Miura-ori sheet and its application: Aerodynamic drag and RCS reduction. Chinese Journal of Aeronautics, 2022, 35(8): 121-131. https://doi.org/10.1016/j.cja.2021.08.004

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Received: 02 March 2021
Revised: 26 April 2021
Accepted: 24 May 2021
Published: 15 September 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).