High-Order Stabilized Finite Elements on Dynamic Meshes
Author:
Affiliation:
1. NASA Langley Research Center
2. University of Tennessee, Chattanooga
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1307
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1. Scalable Implicit Flow Solver for Realistic Wing Simulations with Flow Control
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3. Finite element methods for flow problems with moving boundaries and interfaces
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