NASA NTRS · 19790017897
Feasibility study for a numerical aerodynamic simulation facility. Volume 1
Abstract
A 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.
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Lincoln, N. R., Bergman, R. O., Bonstrom, D. B., Brinkman, T. W., Chiu, S. H. J., Green, S. S., Hansen, S. D., Klein, D. L., Krohn, H. E., Prow, R. P.. 1979-05-01. Feasibility study for a numerical aerodynamic simulation facility. Volume 1. https://ntrs.nasa.gov/citations/19790017897
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