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Probabilistic structural analysis methodology and applications to advanced space propulsion system componentsThe goal of the reported work is to develop and apply new technology that will enable the designer to efficiently and accurately account for each of the design sources of uncertainty as it might affect structural reliability and risk assessment. The paper discusses the development of the Numerical Evaluation of Stochastic Structures Under Stress (NESSUS) finite element code and its supporting reliability algorithms. The NESSUS code and the elements of the solution strategy are outlined and applications are made to several propulsion system components.
Document ID
19910058101
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cruse, T. A.
(Vanderbilt University Nashville, TN, United States)
Rajagopal, K. R.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Dias, J. B.
(Stanford University CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Publication Information
Publication: Computing Systems in Engineering
Volume: 1
Issue: 4-Feb
ISSN: 0956-0521
Subject Category
Spacecraft Propulsion And Power
Accession Number
91A42724
Funding Number(s)
CONTRACT_GRANT: NAS3-24389
Distribution Limits
Public
Copyright
Other

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