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A vectorization of the jameson-caughey nyu transonic swept-wing computer program flo-22-v1 for the star-100 computer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lambiotte Jr., J. J. Pitts, J. I. Smith, R. E. |
| Copyright Year | 1978 |
| Description | The computer program FLO-22 for analyzing inviscid transonic flow past 3-D swept-wing configurations was modified to use vector operations and run on the STAR-100 computer. The vectorized version described herein was called FLO-22-V1. Vector operations were incorporated into Successive Line Over-Relaxation in the transformed horizontal direction. Vector relational operations and control vectors were used to implement upwind differencing at supersonic points. A high speed of computation and extended grid domain were characteristics of FLO-22-V1. The new program was not the optimal vectorization of Successive Line Over-Relaxation applied to transonic flow; however, it proved that vector operations can readily be implemented to increase the computation rate of the algorithm. |
| File Size | 1126357 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780013107 |
| Archival Resource Key | ark:/13960/t9k40kt0q |
| Language | English |
| Publisher Date | 1978-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Inviscid Flow Transonic Flow Algorithms Swept Wings Directional Control Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
