Aerodynamic Analysis of a Spinning Missile with Dithering Canards
Author:
Affiliation:
1. Eloret Corporation, Sunnyvale, California 94087
2. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.13075
Reference10 articles.
1. An Aerodynamic Analysis of a Spinning Missile with Dithering Canards
2. Rolling airframe missile aerodynamic predictions using a chimera approach for dithering canards
3. Numerical Simulation of Rolling Airframes Using a Multilevel Cartesian Method
4. Numerical Simulation of a Spinning Missile with Dithering Canards Using Unstructured Grids
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