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Probabilistic structural analysis verification studiesThe basic objective of this verification effort is to apply probabilistic structural analysis methods developed and implemented in the Numerical Evaluation of Stochastic Structures Under Stress (NESSUS) code to typical space propulsion components. The chosen typical components are turbine blade, high pressure duct, Lox post, and transfer tube liners. Since analysis options of increasing levels of sophistication are implemented in NESSUS incrementally, the verification efforts are also tailored to have increasing levels of sophistication during the progression of the contract. The current released version of the code is limited to linear structural analysis.
Document ID
19870013353
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rajagopal, K. R.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Lewis Research Center Structural Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Structural Mechanics
Accession Number
87N22786
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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