Modified Unsteady Vortex-Lattice Method to Study Flapping Wings in Hover Flight

Title
Modified Unsteady Vortex-Lattice Method to Study Flapping Wings in Hover Flight
Authors
Keywords
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Journal
AIAA JOURNAL
Volume 51, Issue 11, Pages 2628-2642
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2013-09-13
DOI
10.2514/1.j052262

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