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Reliability Analysis for Composite Laminated Plate Using Hybrid Response Surface Method

복합 반응면 기법을 이용한 복합재 적층판의 신뢰성해석

  • 이석제 (충남대학교 항공우주공학과 대학원) ;
  • 김인걸 (충남대학교 항공우주공학과)
  • Published : 2010.04.30

Abstract

In this paper, the hybrid response surface method(HRSM) is proposed and examined. Hybrid response surface method calculate a approximate model repeatedly based on MPP coordinates. To verify the performance, probability of failure, MPP(Most Probable failure Point) and reliability index are calculated for nonlinear function and composite laminated plate by using reliability analysis method and compared with results by using typical response surface method(RSM). Probability of failure is calculated under the assumption of the nonlinear limit state equation and given failure criterion. The results of proposed method shows performance improvement in estimating the probability of failure.

본 논문에서는 복합 반응면 기법을 제안하고 성능을 고찰하였다. 복합 반응면 기법은 MPP의 좌표를 기준으로 하여 근사모델을 반복 계산하는 기법이다. 성능을 검증하기 위해 비선형 함수와 복합재 적층판에 대하여 신뢰성 해석 기법을 적용하여 파괴확률, MPP(Most Probable failure Point), 신뢰도 지수를 계산하고 일반적인 반응면 기법의 결과와 비교하였다. 파괴확률은 비선형 한계상태식을 가정하고 임의의 파괴 기준을 정의하여 계산하였다. 제안한 복합 반응면 기법을 이용하여 파괴확률을 계산한 결과 일반적인 반응면 기법보다 향상된 성능을 나타내었다.

Keywords

References

  1. 양영순 외, 구조신뢰성 공학, 서울대학교 출판부, 1999.
  2. Long, M. W. and Narciso, J. D., Probabilistic Design Methodology for Composite Aircraft Structures, DOT/FAA/AR-99/2, 1999.
  3. Shin, Y. and Wu, Y-T., "Progressive Importance Sampling Approach for Reliability Analysis," 47th AIAA/ASME/ ASCE/AHS/ASC Conference, 2006.
  4. Fujita, K. and Kounoe Y., "High-Order Polynomial Response Surface with Optimal Selection of Interaction Terms," 11th AIAA/ISSMO Conference, 2006.
  5. Myers, R. H. and Montgomery, D. C., Response Surface Methodology, John Wiley & Sons Inc., 2002.
  6. 김철 외, 공학도를 위한 수치해석, McGraw -Hill, 2004.
  7. Liu, H. and Chen, W., "Probabilistic Sensitivity Analysis Methods for Design under Uncertainty," 10th AIAA/ISSMO Conference, 2004.
  8. Haldar, A. and Mahadevan, S., Reliability Assessment using Stochastic Finite Element Analysis, John Wiley & Sons Inc., 2000.
  9. Sekishiro, M., Venter, G., and Balabanov, V., "Combined Kriging and Gradient- Based Optimization Method," AIAA, 2006.
  10. Swanson, S. R., Introduction to Design and Analysis with Advanced Composite Materials, Prentice-Hall International Inc., 1997.
  11. Park, C., Park, B., Joo, Y., and Kim, I., "Monitoring of Impact Forces on an Aircraft Composite Wing," Proceeding of International Joint Conference of INABIO/SMEBA 2006, Daejeon, Korea, Sept., 2006, pp. 101.
  12. 이석제, 김인걸, 장문호, "다양한 설계 요구조건을 고려한 복합재 평판의 신뢰성 해석," 한국복합재료학회지, 제20권 제 4호, 2007, pp. 25-30.

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