Unsteady Flow Features of a Flapping and Pitching Wing at Low Reynolds Number
Author:
Affiliation:
1. University of Missouri-Rolla
2. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3145
Reference8 articles.
1. Wing Rotation and the Aerodynamic Basis of Insect Flight
2. Propulsive vortical signature of plunging and pitching airfoils
3. Active vorticity control in a shear flow using a flapping foil
4. Efficient foil propulsion through vortex control
5. 5Isaac, K. M., Shivaram, P. and DalBello, T. "Low Re, High α Aerodynamics with Controlled Wing Kinematics," AIAA 2003-4019.
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1. Generating LEVs on Energetically Optimal, Flapping Wing Designs by Modulating Leading Edge Angle;31st AIAA Applied Aerodynamics Conference;2013-06-22
2. Planform and Camber Effects on the Aerodynamics of Low-Reynolds-Number Wings;Journal of Aircraft;2010-03
3. Effect of Camber on Force Generation in Leading Edge/Trailing Edge Switching Hovering Mode;27th AIAA Applied Aerodynamics Conference;2009-06-14
4. Aerodynamics of Flapping and Plunging Wings using Particle Image Velocimetry Measurements;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
5. Low Re, High Alpha Wing Aerodynamics for Micro Air Vehicle Applications;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07
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