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      고받음각에서 기동하는 미사일의 공력-구조 연계 해석 = FLUID-STRUCTURE INTERACTION ANALYSIS FOR HIGH ANGLE OF ATTACK MANEUVER MISSILE

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      https://www.riss.kr/link?id=A76280328

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      다국어 초록 (Multilingual Abstract)

      Computational Fluid Dynamics (CFD) and the Finite Element Method (FEM) are used to perform aerodynamics analysis and structure analysis. For the fluid-structure interaction analysis, each technology should be considered as well. The process of aerodynamics-structure coupled analysis can be applied to various integrated analyses from many research fields.
      In this study, the aerodynamics-structure coupled analysis is performed for the missile at high angle of attack condition through the use of Computational Fluid Dynamics (CFD) and the Finite Element Method (FEM). For this purpose, the aerodynamics-structure coupled analyses procedure for the missile are established. the results of the integrated analysis are compared with rigid geometry of the missile and the effect of the deformation will be addressed.
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      Computational Fluid Dynamics (CFD) and the Finite Element Method (FEM) are used to perform aerodynamics analysis and structure analysis. For the fluid-structure interaction analysis, each technology should be considered as well. The process of aerodyn...

      Computational Fluid Dynamics (CFD) and the Finite Element Method (FEM) are used to perform aerodynamics analysis and structure analysis. For the fluid-structure interaction analysis, each technology should be considered as well. The process of aerodynamics-structure coupled analysis can be applied to various integrated analyses from many research fields.
      In this study, the aerodynamics-structure coupled analysis is performed for the missile at high angle of attack condition through the use of Computational Fluid Dynamics (CFD) and the Finite Element Method (FEM). For this purpose, the aerodynamics-structure coupled analyses procedure for the missile are established. the results of the integrated analysis are compared with rigid geometry of the missile and the effect of the deformation will be addressed.

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      목차 (Table of Contents)

      • 1. 서론
      • 2. 공력-구조 연계방법
      • 3. 해석 방법
      • 4. 결론 및 향후 계획
      • 후기
      • 1. 서론
      • 2. 공력-구조 연계방법
      • 3. 해석 방법
      • 4. 결론 및 향후 계획
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      • 참고문헌
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