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Numerical aerodynamic simulation facility feasibility studyThere were three major issues examined in the feasibility study. First, the ability of the proposed system architecture to support the anticipated workload was evaluated. Second, the throughput of the computational engine (the flow model processor) was studied using real application programs. Third, the availability reliability, and maintainability of the system were modeled. The evaluations were based on the baseline systems. The results show that the implementation of the Numerical Aerodynamic Simulation Facility, in the form considered, would indeed be a feasible project with an acceptable level of risk. The technology required (both hardware and software) either already exists or, in the case of a few parts, is expected to be announced this year. Facets of the work described include the hardware configuration, software, user language, and fault tolerance.
Document ID
19790017901
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
March 1, 1979
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-152285
Report Number: NASA-CR-152285
Accession Number
79N26072
Funding Number(s)
CONTRACT_GRANT: NAS2-9897
PROJECT: RTOP 505-06-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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