Design and Aerodynamic Characterization of Canard Guided Fuze for Dual-Spin Artillery Projectiles
Author:
Affiliation:
1. Indian Institute of Technology Kanpur
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-1105
Reference16 articles.
1. Srivastava, B., CFD analysis and validation of lateral jet control of a missile, p.288. https://doi.org/10.2514/6.1996-288.
2. Landers, M., Hall, L., Auman, L., and Vaughn, M., Deflectable Nose and Canard Controls for a Fin-Stabilized Projectile at Supersonic and Hypersonic Speeds, p.3805. https://doi.org/10.2514/6.2003-3805.
3. Shoesmith, B., Birch, T., Mifsud, M., Meunier, M., and Shaw, S., CFD Analysis of a Supersonic Projectile with Deflectable Nose Control, p.3200. https://doi.org/10.2514/6.2006-3200.
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