Computational Model for the Dynamic Analysis of a Two-Dimensional Airfoil with a Control Surface-Reference-Cited by-同舟云学术

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Computational Model for the Dynamic Analysis of a Two-Dimensional Airfoil with a Control Surface

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

Jiménez Rodrigo¹,Lopez Omar¹

Affiliation:

1. University of the Andes

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3846

Reference15 articles.

1. 1Jacobs, E.N., Ward, K.E., Pinkerton, R.M. "The Characteristics of 78 Related Airfoil Sections from Tests in the Variable-DensityWind Tunnel". NACAReport No. 460, 1933.

2. 2Abbot,I.H.,VonDoenhoff,A.E.,StiversJr.,L.S."SummaryofAirfoilData".NACAReportNo.824,1945.

3. 3Loftin Jr., L.K. "Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil Sections". NACA Report No. 903, 1948.

4. Evaluation of Missile Guidance and Control Systems on a Personal Computer

5. 6Hilton,A."MissileGuidanceSimulator",URL:http://www.suslik.org/Simulator/index.html[cited24November2009]

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