Effect of Aspect Ratio on Aerodynamic Characteristics at Low Reynolds Numbers
Author:
Affiliation:
1. Aerospace Engineering, National Defense Academy, Kanagawa 239-8686, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051915
Reference19 articles.
1. AIAA Education Series;Mueller T. J.,2006
2. Experimental Studies of Separation on a Two-Dimensional Airfoil at Low Reynolds Numbers
3. An Overview of Micro Air Vehicle Aerodynamics
4. Introduction
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