Output-Based Adaptive Meshing Applied to Space Launch System Booster Separation Analysis
Author:
Affiliation:
1. Science and Technology Corporation
2. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3152
Reference14 articles.
1. A parallel multilevel method for adaptively refined Cartesian grids with embedded boundaries
2. Adjoint Error Estimation and Adaptive Refinement for Embedded-Boundary Cartesian Meshes
3. Effects of Jet-Interaction on Pitch Control of a Launch Abort Vehicle
4. Rocket Plume Scaling for Orion Wind Tunnel Testing (Invited)
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