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Grid Generation Issues and CFD Simulation Accuracy for the X33 Aerothermal SimulationsGrid generation issues relating to the simulation of the X33 aerothermal environment using the GASP code are explored. Required grid densities and normal grid stretching are discussed with regards to predicting the fluid dynamic and heating environments with the desired accuracy. The generation of volume grids is explored and includes discussions of structured grid generation packages such as GRIDGEN, GRIDPRO and HYPGEN. Volume grid manipulation techniques for obtaining desired outer boundary and grid clustering using the OUTBOUND code are examined. The generation of the surface grid with the required surface grid with the required surface grid topology is also discussed. Utilizing grids without singular axes is explored as a method of avoiding numerical difficulties at the singular line.
Document ID
20020050562
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Polsky, Susan
(Thermoscience Inst. Moffett Field, CA United States)
Papadopoulos, Periklis
(Thermoscience Inst. Moffett Field, CA United States)
Davies, Carol
(NASA Ames Research Center Moffett Field, CA United States)
Loomis, Mark
(NASA Ames Research Center Moffett Field, CA United States)
Prabhu, Dinesh
(Thermoscience Inst. Moffett Field, CA United States)
Langhoff, Stephen R.
Date Acquired
August 20, 2013
Publication Date
January 1, 1997
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 36th AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 12, 1998
End Date: January 15, 1998
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 242-33-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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