A dual-level parallel procedure is presented for computing large databases to support aerospace vehicle design. This procedure has been developed as a single Unix script within the Parallel Batch Submission environment utilizing MPIexec and runs MPI based analysis software. It has been developed to provide a process for aerospace designers to generate data for large numbers of cases with the highest possible fidelity and reasonable wall clock time. A single job submission environment has been created to avoid keeping track of multiple jobs and the associated system administration overhead. The process has been demonstrated for computing large databases for the design of typical aerospace configurations, a launch vehicle and a rotorcraft.


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    Titel :

    Computations on Wings With Full-Span Oscillating Control Surfaces Using Navier-Stokes Equations


    Beteiligte:

    Erscheinungsdatum :

    2013


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Navier-Stokes Computations on a Full-Span Wing-Body Configuration with Oscillating Control Surfaces

    Obayashi, S. / Chiu, I.-T. / Guruswamy, G. et al. | British Library Conference Proceedings | 1993



    Navier-Stokes computations for oscillating control surfaces

    Obayashi, Shigeru / Guruswamy, Guru P. | AIAA | 1994


    Navier-Stokes computations for oscillating control surfaces

    OBAYASHI, SHIGERU / GURUSWAMY, GURU | AIAA | 1992