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Computational simulation for concurrent engineering of aerospace propulsion systemsResults are summarized for an investigation to assess the infrastructure available and the technology readiness in order to develop computational simulation methods/software for concurrent engineering. These results demonstrate that development of computational simulation methods for concurrent engineering is timely. Extensive infrastructure, in terms of multi-discipline simulation, component-specific simulation, system simulators, fabrication process simulation, and simulation of uncertainties--fundamental to develop such methods, is available. An approach is recommended which can be used to develop computational simulation methods for concurrent engineering of propulsion systems and systems in general. Benefits and issues needing early attention in the development are outlined.
Document ID
19930014557
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Singhal, S. N.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-106029
E-7592
NAS 1.15:106029
Meeting Information
Meeting: 1992 AIAA Aerospace Design Conference
Location: Irvine, CA
Country: United States
Start Date: February 3, 1992
End Date: February 6, 1992
Accession Number
93N23746
Funding Number(s)
PROJECT: RTOP 323-57-40
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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