• DocumentCode
    2288581
  • Title

    Dynamic risk assessment of CFD codes [aerospace design]

  • Author

    Wesley, Leonard P. ; Childs, Robert E.

  • Author_Institution
    Comput. Eng. Dept., San Jose State Univ., CA, USA
  • Volume
    7
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    536725
  • Abstract
    The results of an innovative effort to dynamically extract risk measures that can be factored into the knowledge-base closed-loop control of flow calculations is presented. Example control decisions include changing flow-solving parameters or restarting from previous checkpoints to reduce the need for manual intervention. One significance of the work is a formal, rigorous, yet practical KB means to dynamically control the execution of CFD codes by interpreting solution metrics within the context of larger project-related factors. Such factors include the desired solution fidelity, resource limitations such as budget and time, and related previously completed computational fluid dynamics (CFD) analyses. A measure of the risk associated with continuing, changing, or stopping flow calculations is developed in a manner that can be considered when deliberating if, how, and when to change flow calculations. We demonstrate the benefits of extracting and factoring in measures of risk when controlling the execution of CFD codes.
  • Keywords
    CAD; aerospace computing; closed loop systems; computational fluid dynamics; risk management; aerospace community; aerospace design; computational fluid dynamics; dynamic risk assessment; flow-solving parameters; knowledge-base closed-loop control; project-related factors; resource limitations; risk measures; solution fidelity; solution metrics; Aerodynamics; Computational fluid dynamics; Educational institutions; Fluid flow control; Fluid flow measurement; Humans; Knowledge engineering; Risk management; Software systems; Technological innovation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1035315
  • Filename
    1035315