Development of a grid generator to support 3-D multizone Navier-Stokes analysis
Abstract
A three-dimensional grid generation code has been developed to support multizone Navier-Stokes analysis of flowfields associated with complex geometries. The code includes a number of features necessary for this task, including the definition of arbitrary zonal boundary surfaces using the output from a separate surface geometry program. The interior of each zone is gridded by an efficient parabolic/elliptic partial differential equation algorithm. To test the new grid generation code, grids were successfully generated for a finned missile configuration, for a hypersonic vehicle, for a fluid dynamic vortex valve, and for a three-dimensional rocket base/nozzle/plume configuration. Navier-Stokes calculations were run on these grids, with satisfactory results. The new code is expected to provide a solid basis for the extension to optimized and solution-adaptive grid generation in the future.
- Publication:
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25th AIAA Aerospace Sciences Meeting
- Pub Date:
- January 1987
- Bibcode:
- 1987aiaa.meetS....H
- Keywords:
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- Computational Fluid Dynamics;
- Computational Grids;
- Grid Generation (Mathematics);
- Navier-Stokes Equation;
- Hypersonic Vehicles;
- Missile Configurations;
- Nozzle Design;
- Orthogonality;
- Vortices;
- Fluid Mechanics and Heat Transfer