Computational Fluid Dynamics and Experimental Data Comparison of a Missile-Model Roll Derivative
Author:
Affiliation:
1. University of Defence, 11000 Belgrade, Serbia
2. Military Technical Institute, 11000 Belgrade, Serbia
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.A33674
Reference16 articles.
1. A simple estimation procedure of roll-rate derivatives for finned vehicles
2. 2009 Version of the Aeroprediction Code: AP09
3. Rapid Computation of Dynamic Stability Derivatives
4. Prediction of Damping Coefficients Using the Unsteady Euler Equations
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