Journal of Aerospace System Engineering (항공우주시스템공학회지)
- Volume 6 Issue 4
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- Pages.1-6
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- 2012
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
DOI QR Code
Static Aeroelastic analysis of Morphing flap wign through FSI analysis method
FSI를 이용한 모핑 플랩 날개의 정적 공탄성 해석
- Received : 2012.11.16
- Accepted : 2012.12.18
- Published : 2012.12.31
Abstract
The morphing flap wing has different structure unliked general wing structure. The actuated chord length of the morphing flap was more longer than conventional wing flap. In this reason, morphing flap wing structure was important to bending moment by aerodynamic lift force. In this study, through the fluid-structure interaction using computational fluid dynamics and structure finite element analysis to apply that the morphing flap wing's static aeroelastic stability analysis.
Keywords
- Morphing Wing;
- FSI(Fluid-Structure Interaction);
- CFD(Computational Fluid Dynamics);
- FEM(Finite Element Method)