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Structural reliability methods: Code development statusThe Probabilistic Structures Analysis Method (PSAM) program integrates state of the art probabilistic algorithms with structural analysis methods in order to quantify the behavior of Space Shuttle Main Engine structures subject to uncertain loadings, boundary conditions, material parameters, and geometric conditions. An advanced, efficient probabilistic structural analysis software program, NESSUS (Numerical Evaluation of Stochastic Structures Under Stress) was developed as a deliverable. NESSUS contains a number of integrated software components to perform probabilistic analysis of complex structures. A nonlinear finite element module NESSUS/FEM is used to model the structure and obtain structural sensitivities. Some of the capabilities of NESSUS/FEM are shown. A Fast Probability Integration module NESSUS/FPI estimates the probability given the structural sensitivities. A driver module, PFEM, couples the FEM and FPI. NESSUS, version 5.0, addresses component reliability, resistance, and risk.
Document ID
19930022374
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Millwater, Harry R.
(Southwest Research Inst. San Antonio, TX, United States)
Thacker, Ben H.
(Southwest Research Inst. San Antonio, TX, United States)
Wu, Y.-T.
(Southwest Research Inst. San Antonio, TX, United States)
Cruse, T. A.
(Vanderbilt Univ. Nashville, TN., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA. Lewis Research Center, Structural Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Quality Assurance And Reliability
Accession Number
93N31563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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