항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제6권4호
  • /
  • Pages.1-6
  • /
  • 2012
  • /
  • 1976-6300(pISSN)
  • /
  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
권호 표지
DOI QR코드

DOI QR Code

FSI를 이용한 모핑 플랩 날개의 정적 공탄성 해석

Static Aeroelastic analysis of Morphing flap wign through FSI analysis method

  • 김종환 (한국항공대학교 항공우주공학과) ;
  • 고승희 (한국항공대학교 항공우주공학과) ;
  • 배재성 (한국항공대학교 항공우주공학과) ;
  • 투고 : 2012.11.16
  • 심사 : 2012.12.18
  • 발행 : 2012.12.31
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

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.

키워드