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Matrix Structure Reliability Analysis using AFORM

개선된 일계이차모멘트법을 적용한 메트릭스 구조물 신뢰도 해석

  • Received : 2012.08.17
  • Accepted : 2012.09.19
  • Published : 2012.09.30

Abstract

The wing is a framework composed chiefly of skin, spars, ribs and can be simplified by matrix structure. In this paper, a displacement reliability of matrix structure is analysed by AFORM(Advanced First Order Reliability Method) and applicability is assessed.

References

  1. Achintya Haldar and Sankaran Mahadevan, "Reliability Assessment Using Stochastic Finite Element Analysis", John Wiley & Sons, INC.
  2. Achintya Haldar and Sankaran Mahadevan, "Probability, Reliability and Statistical Method in Engineering Design", John Wiley & Sons, INC.
  3. 양영순, 서용석, 이재옥, "구조 신뢰성 공학", 서울대학교 출판부
  4. Richard H. Gallagher, Ivan Rattinger and John S. Archer, "A Correlation Study of Methods of Matrix Structural Analysis", Pergamon Press