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Feasibility study for a numerical aerodynamic simulation facility. Volume 1A Numerical Aerodynamic Simulation Facility (NASF) was designed for the simulation of fluid flow around three-dimensional bodies, both in wind tunnel environments and in free space. The application of numerical simulation to this field of endeavor promised to yield economies in aerodynamic and aircraft body designs. A model for a NASF/FMP (Flow Model Processor) ensemble using a possible approach to meeting NASF goals is presented. The computer hardware and software are presented, along with the entire design and performance analysis and evaluation.
Document ID
19790017897
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lincoln, N. R. (Control Data Corp. Saint Paul, MN, United States)
Bergman, R. O. (Control Data Corp. Saint Paul, MN, United States)
Bonstrom, D. B. (Control Data Corp. Saint Paul, MN, United States)
Brinkman, T. W. (Control Data Corp. Saint Paul, MN, United States)
Chiu, S. H. J. (Control Data Corp. Saint Paul, MN, United States)
Green, S. S. (Control Data Corp. Saint Paul, MN, United States)
Hansen, S. D. (Control Data Corp. Saint Paul, MN, United States)
Klein, D. L. (Control Data Corp. Saint Paul, MN, United States)
Krohn, H. E. (Control Data Corp. Saint Paul, MN, United States)
Prow, R. P. (Control Data Corp. Saint Paul, MN, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1979
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-152287
Report Number: NASA-CR-152287
Accession Number
79N26068
Funding Number(s)
CONTRACT_GRANT: NAS2-9896
PROJECT: RTOP 505-06-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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