Basic HTML version of Foils prepared 15 March 1996

Foil 21 NASA's Estimate of Computing Needs for Reynolds Averaged Approximation (1994)

From Overview of CFD and Numerical Relativity Case Study CPSP713 -- Autumn Semester 1994. by Geoffrey C. Fox
1 Flow Simulation ( Reynolds Averaged Approximation ):
  • 5x106 grid points
  • 5x104 iterations
  • 5x103 operations/iterations
  • 1015 operations (flops) / problem
  • 2x108 words of memory
    • Hours GigaFlops
2 Proof of concept 1000-->100 0.3-->3
  • Design 10-->1 30-->300
3 Automated Design 0.1-->0.01 3000-->30,000
in Table To:

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