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Preliminary study for a Numerical Aerodynamic Simulation FacilityThe state of the art of relevant technologies, of systems and processor architectures, and the measurable computational requirements of the two existing Navier-Stokes solution programs were assessed by Control Data Corporation to determine the best approach for designing a system for aerodynamic simulation. Standard parts and components were used to identify the support processing system, which is composed of commercially available equipment and software. Technological achievements in large scale integration technology and system organization of subcomponents borrowed from the STAR-100C project were used in the design of the Navier-Stokes solver.
Document ID
19780011840
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lincoln, N. R.
(Control Data Corp. Minneapolis, MN, United States)
Date Acquired
August 9, 2013
Publication Date
February 1, 1978
Publication Information
Publication: NASA. Ames Res. Center Future Computer Requirements for Computational Aerodynamics
Subject Category
Computer Programming And Software
Accession Number
78N19783
Funding Number(s)
CONTRACT_GRANT: NAS2-9457
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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