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Numerical computation of complex multi-body Navier-Stokes flows with applications for the integrated Space Shuttle launch vehicleAn enhanced grid system for the Space Shuttle Orbiter was built by integrating CAD definitions from several sources and then generating the surface and volume grids. The new grid system contains geometric components not modeled previously plus significant enhancements on geometry that has been modeled in the old grid system. The new orbiter grids were then integrated with new grids for the rest of the launch vehicle. Enhancements were made to the hyperbolic grid generator HYPGEN and new tools for grid projection, manipulation, and modification, Cartesian box grid and far field grid generation and post-processing of flow solver data were developed.
Document ID
19930011578
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chan, William M.
(MCAT Inst. San Jose, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:192297
MCAT-93-05
NASA-CR-192297
Report Number: NAS 1.26:192297
Report Number: MCAT-93-05
Report Number: NASA-CR-192297
Accession Number
93N20767
Funding Number(s)
CONTRACT_GRANT: NCC2-654
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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