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4 edition of Final report for parallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997 found in the catalog.

Final report for parallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997

Final report for parallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997

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Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va .
Written in English

    Subjects:
  • Parallel computers,
  • Unsteady flow,
  • Management systems,
  • Data smoothing,
  • Computational fluid dynamics

  • Edition Notes

    Other titlesParallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997
    Series[NASA contractor report] -- NASA CR-206142.
    ContributionsUnited States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17822427M
    OCLC/WorldCa38840583

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Final report for parallel computation of unsteady flows on a network of workstations (NAG3-1577) for the period of 1993-1997 Download PDF EPUB FB2

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Parallel Computational Fluid Dynamics Implementations and Results Using Parallel Computers. Parallel computation of unsteady supersonic-inlet flows The parallel code was tested on both a network of workstations and on the Cray torus, three-dimensional (T3D).

The serial NPARC code was successfully parallelized to run in single. A physics-based computational method is presented for the trajectory prediction of fully appended self-propelled underwater vehicles, including a rotating propeller. The approach is to interactively couple the numerical solution of the three-dimensional unsteady incompressible turbulent Navier-Stokes equations with a six-degree-of-freedom (6-DOF) computational method.

where is the Froude number and the Reynolds number Re is defined by where v is the kinematic viscosity, and is a dimensionless form of the Reynolds stress. Figure 1 shows the reference frame and ship location used in this work.

A right-handed coordinate system Oxyz, with the origin fixed at the intersection of the bow and the mean free surface is established. Parallel computation techniques may bring a considerable saving in time in the computer simulation of turbomachinery flows. The program complex is presented for numerical simulation of 3D sufficiently unsteady flows of viscous compressible heat conducting gas.

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Introduction: The CERFACS Parallel Utilities Library (CPULib) The purpose of this paper is to report on recent progress in the development of a complex code for "modular" parallel fluid dynamics.

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and Avila, A.F. and Tamma, K.K. and Namburu, R.R.}, abstractNote = {The recent trend in the computing industry is toward massively parallel.

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The prediction of unsteady separated, low Mach number flows over complex configurations (like ships and helicopter fuselages) is known to be a very difficult problem. The possibility of predicting these types of flows with the aid of inexpensive parallel computers is explored in this work.

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Full text of "An Introduction To Computational Fluid Dynamics" See other formats. Full text of "NASA Technical Reports Server (NTRS) Aeronautical engineering: A continuing bibliography with indexes (supplement )" See other formats.

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