Recent Enhancements to the FUN3D Flow Solver for Moving-Mesh Applications
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1360
Reference41 articles.
1. Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code
2. 5Biedron, R. T., Vatsa, V. N., and Atkins, H. L. "Simulation of Unsteady Flows Using an Unstructured Navier-Stokes Solver on Moving and Stationary Grids," AIAAPaper2005-5093, June2005.
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