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Extensive 3D analysis for fluid–structure interaction of spanwise flexible plunging wing 3D FSI Analysis for Spanwise Flexible Plunging Wing

Published online by Cambridge University Press:  13 March 2019

H. Cho ,
N. Lee ,
S.-J. Shin Open the ORCID record for S.-J. Shin [Opens in a new window]  and
S. Lee
H. Cho*
Affiliation:
BK21 Plus Transformative Training Program for Creative Mechanical and Aerospace Engineers, Institute of Advanced Machines and Design, Seoul National University, Seoul, Republic of Korea
N. Lee*
Affiliation:
R&D Strategy Team, Vehicle & Launcher System R&D Division, Hanwha Defense Systems, Gyeongsangnam-do, Republic of Korea
S.-J. Shin*
Affiliation:
Department of Mechanical and Aerospace Engineering, Institute of Advanced Aerospace Technology, Seoul National University, Seoul, Republic of Korea
S. Lee*
Affiliation:
Department of Aerospace Engineering, Inha University, Incheon, Republic of Korea
*
nicejjo@snu.ac.kr
namhun.lee@hanwha.com
ssjoon@snu.ac.kr
slee@inha.ac.kr
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Abstract

In this study, an improved fluid–structure interaction (FSI) analysis method is developed for a flapping wing. A co-rotational (CR) shell element is developed for its structural analysis. Further, a relevant non-linear dynamic formulation is developed based on the CR framework. Three-dimensional preconditioned Navier–Stokes equations are employed for its fluid analysis. An implicit coupling scheme is employed to combine the structural and fluid analyses. An explicit investigation of a 3D plunging wing is conducted using this FSI analysis method. A further investigation of this plunging wing is performed in relation to its operating condition. In addition, the relation between the wing’s aerodynamic performance and plunging motion is investigated.

Keywords

Fluid–structure interactionSpanwise flexibilityCo-rotational shell
Type
Research Article
Information
The Aeronautical Journal , Volume 123 , Issue 1262 , April 2019 , pp. 484 - 506
Copyright
© Royal Aeronautical Society 2019 

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