Computation of Unsteady Low Reynolds Number Free-Flight Aerodynamics of Flapping Wings
Author:
Affiliation:
1. Nanyang Technological University, Singapore 639798, Republic of Singapore
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.44456
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1. Experimental and Computational Investigation of the Knoller-Betz Effect
2. Unsteady forces and flows in low Reynolds number hovering flight:two-dimensional computationsvsrobotic wing experiments
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