Numerical Computations of Dynamic Derivatives of a Finned Projectile Using A Time-Accurate CFD Method
Author:
Affiliation:
1. U.S. Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6581
Reference30 articles.
1. Meakin, R.L. "Computations of the Unsteady Flow About a Generic Wing/Pylon/Finned-StoreConfiguration."AIAA 92-4568-CP, August 1992.
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