Multi-Fidelity Coupled Trim Analysis of a Flapping-Wing Micro Air Vehicle Flight
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
2. U.S. Army Research Laboratory, Aberdeen Proving Grounds, Maryland 21005
Funder
Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C034236
Reference31 articles.
1. Aerodynamics, sensing and control of insect-scale flapping-wing flight
2. Aerodynamics of Low Reynolds Number Flyers
3. The aerodynamics of hovering insect flight. I. The quasi-steady analysis
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