November 03 (Friday)
CAE 및 응용역학부문 포스터
Poster,
3층 로비,
14:10~15:00
  • Chair :
  •  강건욱(연세대), 강남우(KAIST), 김남근(인천대), 손동우(한국해양대)
Fr16C-48
14:10~15:00
고온고속 환경에서 로켓 가변노즐에 대한 열유체-유연다물체동역학 연성해석 기법 연구
송승민, 조승현, 강동근(건국대학교), 배주현, 박동창(국방과학연구소), 김창완(건국대학교)
Variable nozzle has converging and diverging flap. So it has advantage to change variable cross section area of nozzle throat. Additionally, it can able to control by actuators in nozzle system. This nozzle system operates at high temperature, speed and pressure. Therefore, it is very important to consider structural safety of the nozzle design. Also, if the area of nozzle throat is changed, pressure and temperature fields are also varies. Hence, the interaction analysis between CFD(Computational Fluid Dynamics) and FMBD(Flexible Multi-Body Dynamics) is must be required. In this paper, a study on the variable nozzle system is conducted using CFD-FMBD interaction analysis on environments of high temperature and pressure.
Keywords : CFD-FMBD interaction analysis(열 유체-유연다물체동역학 연성해석), Rocketvariable nozzle(로켓 가변노즐)
Paper : Fr16C-48.pdf

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