Simulation of Aircraft Response to Control Surface Deflection Using Unstructured Dynamic Grids
Author:
Affiliation:
1. Tohoku University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2940
Reference16 articles.
1. Intergrid-Boundary Definition Method for Overset Unstructured Grid Approach
2. Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids
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