2-단계 기포(氣砲)의 성능 최적화에 관한 연구

Performance Optimization of the Two-Stage Gas Gun Based on Experimental Result

  • 이진호 (건국대학교 대학원 항공우주공학과) ;
  • 배기준 (건국대학교 대학원 항공우주공학과) ;
  • 전권수 (건국대학교 대학원 항공우주공학과) ;
  • 변영환 (건국대학교 대학원 항공우주공학과) ;
  • 이재우 (건국대학교 대학원 항공우주공학과) ;
  • 허철준 (서울대학교 대학원 항공우주공학과)
  • 발행 : 2003.10.01

초록

The present study aims to optimize the performance of the Two-Stage Gas Gun by using the experimentally obtained data. RSM(Response Surface Method) was adopted in the optimization process to find the operating parameter than can maximize the projectile speed with the minimum number of tests. To decide the test points which results can consist of the response surface, 3$^{k}$ full factorial method was used, and the design variables were chosen with piston mass and 2$^{nd}$ driver fill pressure. The response surface was composed by nine test results and consequently the optimization was done with GENOCOP III, inherently GA code, in order to seek the optimal test point. The optimal test condition from the response surface was verified by the experiment. Results showed that the optimization process with response surface can successfully predict the test results fairly well. This study shows the possibility of performance optimization for the experimental facilities using numerical optimization algorithm.

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