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Parallel Computational Fluid Dynamics 2007 pp 83–90Cite as

Efficient Parallel Algoritm for multiconstrained of wing body configurations

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Part of the book series: Lecture Notes in Computational Science and Engineering ((LNCSE,volume 67))

Abstract

It is generally expected in aircraft industry that automatic or even semi-automatic optimizers may essentially shorten the process of aerodynamic design, design, especially at the preliminary design stage, which may cost above 100 million USD [1]. Alongside the reduction in the design costs, accurate optimizers may imporve the quality of design making the project more competitive.

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References

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Authors and Affiliations

  1. Israel Aircraft Industries, Israel

    S. Peigin

  2. The Academic College of Tel-Aiv Yaffo, Israel

    B. Epstein

Authors
  1. S. Peigin
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  2. B. Epstein
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© 2009 Springer-Verlag Berlin Heidelberg

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Peigin, S., Epstein, B. (2009). Efficient Parallel Algoritm for multiconstrained of wing body configurations. In: Parallel Computational Fluid Dynamics 2007. Lecture Notes in Computational Science and Engineering, vol 67. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-92744-0_10

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