Numerical Analysis on Aerodynamic Force Generation of Biplane Counter-Flapping Flexible Airfoils
Author:
Affiliation:
1. National Defense University, Tao-Yuan 355, Taiwan, Republic of China
2. National Pingtung University of Science and Technology, Pingtung 912, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.43181
Reference25 articles.
1. The aerodynamics of hovering insect flight. I. The quasi-steady analysis
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5. Unsteady forces and flows in low Reynolds number hovering flight:two-dimensional computationsvsrobotic wing experiments
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