NASA NTRS · 19780002178
Numerical aerodynamic simulation facility preliminary study: Executive study
Abstract
A computing system was designed with the capability of providing an effective throughput of one billion floating point operations per second for three dimensional Navier-Stokes codes. The methodology used in defining the baseline design, and the major elements of the numerical aerodynamic simulation facility are described.
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1977-10-01. Numerical aerodynamic simulation facility preliminary study: Executive study. https://ntrs.nasa.gov/citations/19780002178
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