Numerical Simulation of a Spinning Missile with Dithering Canards Using Unstructured Grids
Author:
Affiliation:
1. Mississippi State University, Mississippi State, Mississippi 39762-9627
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.9197
Reference10 articles.
1. Chimera Moving Body Methodology for Rolling Airframe Missile Simulation with Dithering Canards
2. Efficient Generation of High-Quality Unstructured Surface and Volume Grids
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