A Vectorization of the Jameson-Caughey Nyu Transonic Swept-Wing Computer Program Flo-22-V1 for the Star-100 Computer
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. Smith, R. E. and Pitts, J. I. and Lambiotte, J. J., Jr. Langley Research Center NASA-TM-78665
32 pages
English edition · First published 2018 by CreateSpace Independent Publishing Platform · ISBN 9781724224804
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