NASA NTRS · 20030066152
Automated CFD Database Generation for a 2nd Generation Glide-Back-Booster
Abstract
A new software tool, AeroDB, is used to compute thousands of Euler and Navier-Stokes solutions for a 2nd generation glide-back booster in one week. The solution process exploits a common job-submission grid environment using 13 computers located at 4 different geographical sites. Process automation and web-based access to the database greatly reduces the user workload, removing much of the tedium and tendency for user input errors. The database consists of forces, moments, and solution files obtained by varying the Mach number, angle of attack, and sideslip angle. The forces and moments compare well with experimental data. Stability derivatives are also computed using a monotone cubic spline procedure. Flow visualization and three-dimensional surface plots are used to interpret and characterize the nature of computed flow fields.
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Chaderjian, Neal M., Rogers, Stuart E., Aftosmis, Michael J., Pandya, Shishir A., Ahmad, Jasim U., Tejmil, Edward. 2003-01-01. Automated CFD Database Generation for a 2nd Generation Glide-Back-Booster. https://ntrs.nasa.gov/citations/20030066152
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