원심 압축기 임펠러의 최적 구조 설계

Optimum Structural Design for Centrifugal Compressor Impeller

  • 최유진 (서울대학교 대학원 항공우주공학과) ;
  • 송준영 (서울대학교 대학원 항공우주공학과) ;
  • 김승조 (서울대학교 기계항공공학부) ;
  • 강신형 (서울대학교 기계항공공학부)
  • 발행 : 1999.12.01

초록

Using basic shape and aerodynamic data for the designed impeller, basic structure analysis such as stress analysis and eigenvalue analysis was carried out. Also, we made the optimization program that was designed for optimum thickness within the adaptive stress limits. For the structural optimum theory, we used the BFGS(Broydon Fletcher Goldfarb Shanno) Method which is one of the searching methods. Through this program we managed optimization of the blade. For numerical simulation, we used the optimization program to compose Cyclic Module of NASTRAN and the Optimization Program which was implemented by C and fortran language.

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