Flight Behaviors of a Complex Projectile using a Coupled CFD-based Simulation Technique: Closed-loop Control
Author:
Affiliation:
1. Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4332
Reference30 articles.
1. Numerical Computations of Dynamic Derivatives of a Finned Projectile Using A Time-Accurate CFD Method
2. Navier-Stokes Computations for a Spinning Projectile from Subsonic to Supersonic Speeds
3. Lateral Jet Interaction on a Finned Projectile in Supersonic Flow
4. Time-Accurate Computations for Rapid Generation of Missile Aerodynamics
5. Optimized Guidance of a Supersonic Projectile Using Pin Based Actuators
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