Aerodynamic Ground Effects of a Tailless Chevron-Shaped UCAV Model-Reference-Cited by-同舟云学术

Aerodynamic Ground Effects of a Tailless Chevron-Shaped UCAV Model

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA Applied Aerodynamics Conference
language:
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Author:

Jones Brett¹,Franke Milton¹,Stephen Eric¹

Affiliation:

1. Air Force Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2832

Reference40 articles.

1. 1Reed, S. A., Subsonic Aerodynamic Stability and Control Assessment of Advanced Aerial Vehicle Configurations, MS thesis, SchoolofGraduateStudies,WrightstateUniversity, Dayton,OH, March1998.

2. 3Buell, D. A., Tinling, B. E. "Ground Effects on the Longitudinal Characteristics of Two Models with Wings Having Low Aspect Ratio andPointedTips".NACA TN 4044,1957.

3. 4Ranzenbach, R., Barlow, J. B., and Diaz, R. H. "Multi-Element Airfoil in Ground Effect - An Experimental and ComputationalStudy", Paper No.AIAA-97-2238, January1997.

4. 5Fink, M.P., Lastinger J. L. "Aerodynamic Characteristics of Low-Aspect-Ratio Wings in Close Proximity to the Wall", NASA TN D-926,1961.

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