Experiences with explicit finite-difference schemes for complex fluid dynamics problems on STAR-100 and CYBER-203 computers
Abstract
Several two- and three-dimensional external and internal flow problems solved on the STAR-100 and CYBER-203 vector processing computers are described. The flow field was described by the full Navier-Stokes equations which were then solved by explicit finite-difference algorithms. Problem results and computer system requirements are presented. Program organization and data base structure for three-dimensional computer codes which will eliminate or improve on page faulting, are discussed. Storage requirements for three-dimensional codes are reduced by calculating transformation metric data in each step. As a result, in-core grid points were increased in number by 50% to 150,000, with a 10% execution time increase. An assessment of current and future machine requirements shows that even on the CYBER-205 computer only a few problems can be solved realistically. Estimates reveal that the present situation is more storage limited than compute rate limited, but advancements in both storage and speed are essential to realistically calculate three-dimensional flow.
- Publication:
-
NASA STI/Recon Technical Report A
- Pub Date:
- August 1982
- Bibcode:
- 1982STIA...8243251K
- Keywords:
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- Cdc Cyber 203 Computer;
- Computational Fluid Dynamics;
- Computer Systems Performance;
- Finite Difference Theory;
- Navier-Stokes Equation;
- Vector Analysis;
- Computer Programs;
- Computer Storage Devices;
- Data Bases;
- Inlet Flow;
- Subsonic Flow;
- Supersonic Combustion Ramjet Engines;
- Three Dimensional Flow;
- Two Dimensional Flow;
- User Requirements;
- Fluid Mechanics and Heat Transfer