Aspect-Ratio Effects on Aeromechanics of Membrane Wings at Moderate Reynolds Numbers
Author:
Affiliation:
1. Aerodynamics and Flight Mechanics Group, University of Southampton, Southampton, England SO17 1BJ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053522
Reference29 articles.
1. Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil
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