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- W1639041711 abstract "The results of a research activity aimed at providing a finite element capability for analyzing turbo-machinery bladed-disk assemblies in a vector/parallel processing environment are summarized. Analysis of aircraft turbofan engines is very computationally intensive. The performance limit of modern day computers with a single processing unit was estimated at 3 billions of floating point operations per second (3 gigaflops). In view of this limit of a sequential unit, performance rates higher than 3 gigaflops can be achieved only through vectorization and/or parallelization as on Alliant FX/80. Accordingly, the efforts of this critically needed research were geared towards developing and evaluating parallel finite element methods for static and vibration analysis. A special purpose code, named with the acronym SAPNEW, performs static and eigen analysis of multi-degree-of-freedom blade models built-up from flat thin shell elements." @default.
- W1639041711 created "2016-06-24" @default.
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- W1639041711 date "1992-02-01" @default.
- W1639041711 modified "2023-09-23" @default.
- W1639041711 title "SAPNEW: Parallel finite element code for thin shell structures on the Alliant FX/80" @default.
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