NASA NTRS · 20100024103
Computations of Aerodynamic Performance Databases Using Output-Based Refinement
Abstract
Objectives: Handle complex geometry problems; Control discretization errors via solution-adaptive mesh refinement; Focus on aerodynamic databases of parametric and optimization studies: 1. Accuracy: satisfy prescribed error bounds 2. Robustness and speed: may require over 105 mesh generations 3. Automation: avoid user supervision Obtain "expert meshes" independent of user skill; and Run every case adaptively in production settings.
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Nemec, Marian, Aftosmis, Michael J.. 2009-01-11. Computations of Aerodynamic Performance Databases Using Output-Based Refinement. https://ntrs.nasa.gov/citations/20100024103
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