Enhanced Body Vortex Modeling Within Missile Datcom
Author:
Affiliation:
1. Army Aviation and Missile Research Development and Engineering Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2587
Reference17 articles.
1. Fin-Shed Vortex Modeling Within Missile Datcom
2. Improved Validation Methodology for Missile Datcom Development
3. Pitts, W. C., Nielsen, J. N., Kaattari, G. E. "Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds," NACA Report 1307, 1957.
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