This paper describes a concurrent implementation of the Aerospace Launch System Implicit/Explicit Navier-Stokes code (ALSINS). This general code is the primary tool used by The Aerospace Corporation for comlex multi-body launch vehicle configurations and nozzle flow calculations. The code utilizes a finite volume TVD scheme for computing both steady state and unsteady solutions to the 3-D compressible Navier-Stokes equations.


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    Title :

    A concurrent Navier-Stokes solver for implicit multibody calculations


    Additional title:

    Ein paralleles Navier-Stokes-Lösungsverfahren für impliziete Mehrkörperberechnungen


    Contributors:
    Wang, J.C.T. (author) / Taylor, S. (author)


    Publication date :

    1995


    Size :

    11 Seiten, 4 Bilder, 10 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English