- Volume 20 Issue 3
DOI QR Code
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
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.
- Achintya Haldar and Sankaran Mahadevan, "Reliability Assessment Using Stochastic Finite Element Analysis", John Wiley & Sons, INC.
- Achintya Haldar and Sankaran Mahadevan, "Probability, Reliability and Statistical Method in Engineering Design", John Wiley & Sons, INC.
- 양영순, 서용석, 이재옥, "구조 신뢰성 공학", 서울대학교 출판부
- Richard H. Gallagher, Ivan Rattinger and John S. Archer, "A Correlation Study of Methods of Matrix Structural Analysis", Pergamon Press