Design of Flapping Airfoil for Optimal Aerodynamic Performance in Low-Reynolds Number Flows
Author:
Affiliation:
1. Seoul National University, Seoul 151-742, Republic of Korea
2. Institute of Advanced Aerospace Technology, Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.15981
Reference16 articles.
1. Numerical computation of flapping-wing propulsion and power extraction
2. An experimental and numerical investigation of flapping-wing propulsion
3. Vortical patterns in the wake of an oscillating airfoil
4. Oscillating foils of high propulsive efficiency
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