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  • 1
    Publication Date: 2013-08-31
    Description: Algorithms are described for the generation and adaptation of unstructured grids in two and three dimensions, as well as Euler solvers for unstructured grids. The main purpose is to demonstrate how unstructured grids may be employed advantageously for the economic simulation of both geometrically as well as physically complex flow fields.
    Keywords: AERODYNAMICS
    Type: Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1; p 377-408
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-28
    Description: A set of computer programs for 3-D unstructured grid generation, fluid flow calculations, and flow field visualization was developed. The grid generation program, called VGRID3D, generates grids over complex configurations using the advancing front method. In this method, the point and element generation is accomplished simultaneously, VPLOT3D is an interactive, menudriven pre- and post-processor graphics program for interpolation and display of unstructured grid data. The flow solver, VFLOW3D, is an Euler equation solver based on an explicit, two-step, Taylor-Galerkin algorithm which uses the Flux Corrected Transport (FCT) concept for a wriggle-free solution. Using these programs, increasingly complex 3-D configurations of interest to aerospace community were gridded including a complete Space Transportation System comprised of the space-shuttle orbitor, the solid-rocket boosters, and the external tank. Flow solutions were obtained on various configurations in subsonic, transonic, and supersonic flow regimes.
    Keywords: AERODYNAMICS
    Type: NASA-CR-182090 , NAS 1.26:182090
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-12
    Keywords: NUMERICAL ANALYSIS
    Type: International Journal for Numerical Methods in Fluids (ISSN 0271-2091); 8; 1135-114
    Format: text
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  • 4
    Publication Date: 2019-07-13
    Description: Some algorithmic problems encountered during the development of unstructured grid plotting codes are described. Chief among them are the interpolation of three-dimensional data on planes, the plotting of a three-dimensional surface with a constant value for a given unknown, and the calculation of particle and oil-flow paths. Some special features of the unstructured grid plotting code, FEPLOT3D, are also described.
    Keywords: NUMERICAL ANALYSIS
    Type: AIAA PAPER 89-1981 , AIAA Computational Fluid Dynamics Conference; Jun 13, 1989 - Jun 15, 1989; Buffalo, NY; United States
    Format: text
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