Fin-Shed Vortex Modeling Within Missile Datcom-Reference-Cited by-同舟云学术

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Fin-Shed Vortex Modeling Within Missile Datcom

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Rosema Christopher¹,Doyle Joshua²

Affiliation:

1. U.S. Army Aviation and Missile Research Development and Engineering Center

2. Dynetics, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1240

Reference12 articles.

1. 1Doyle,J.B.,Rosema,C.C.,et.al,"ImprovementsinFin-ShedVortexTreatmentforMissileDatcom,"AIAA09-3853,June 2009.

2. 5Pitts, W. C., Nielsen, J. N., and Kaattari, G. E, "Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, andSupersonicSpeeds,"NACAReport 1307,1957.

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