Computation of the roll characteristics of a finned projectile
Author:
Affiliation:
1. U.S. Army Research Laboratory, Aberdeen Proving Ground, Maryland 21005-5066
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26836
Reference15 articles.
1. Multiple-zone strategy for supersonic missiles
2. Prediction of Roll Moments on Finned Bodies in Supersonic Flow
3. A simple estimation procedure of roll-rate derivatives for finned vehicles
4. Roll damping of cruciform-tailed missiles
5. Roll damping for projectiles including wraparound, offset, and arbitrary number of fins
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2. High-Alpha Prediction of Roll Damping and Magnus Stability Coefficients for Finned Projectiles;Journal of Spacecraft and Rockets;2016-07
3. Comparison of Uncoupled and Coupled CFD-based Simulation Techniques for the Prediction of the Aerodynamic Behavior of a Complex Projectile;34th AIAA Applied Aerodynamics Conference;2016-06-10
4. Numerical Experiments on Finned Bodies;32nd AIAA Applied Aerodynamics Conference;2014-06-13
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