• DocumentCode
    1920987
  • Title

    Aerodynamics Analysis Acceleration through Reconfigurable Hardware

  • Author

    Andres, E. ; Molina, M. ; Botella, G. ; del Barrio, A. ; Mendias, J.

  • Author_Institution
    Dipt. Arquitectura de Comput. y Autom., Univ. Complutense de Madrid, Madrid
  • fYear
    2008
  • fDate
    26-28 March 2008
  • Firstpage
    105
  • Lastpage
    110
  • Abstract
    The long computation times required to simulate complete aircraft configurations remain as the main bottleneck in the design flow of new structures for the aeronautics industry. In this paper, the novel application of specific hardware in conjunction with conventional processors to accelerate Computational fluid dynamics is explored. First, some general facts about application-specific hardware are presented, placing the focus on the feasibility of the development of hardware modules (FPGAs based) for the acceleration of most time-consuming algorithms in aeronautics analysis. So, a practical methodology for developing an FPGA- based computing solution for the quasi ID Euler equations is applied to the Sod\´s "shock tube" problem. Results comparing CPU-based and FPGA-based solutions are presented, showing that speedups around two orders of magnitude can be expected from the FPGA-based implementation.
  • Keywords
    aerodynamics; aerospace engineering; aircraft testing; computational fluid dynamics; field programmable gate arrays; FPGA-based computing; aerodynamics analysis acceleration; aeronautics industry; aircraft configuration; computational fluid dynamics; quasi 1D Euler equation; reconfigurable hardware; Acceleration; Aerodynamics; Aerospace industry; Aircraft; Algorithm design and analysis; Computational fluid dynamics; Computational modeling; Computer industry; Field programmable gate arrays; Hardware;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Programmable Logic, 2008 4th Southern Conference on
  • Conference_Location
    San Carlos de Bariloche
  • Print_ISBN
    978-1-4244-1992-0
  • Type

    conf

  • DOI
    10.1109/SPL.2008.4547740
  • Filename
    4547740