Parametric Variations in Aspect Ratio, Leading Edge and Planform Shapes for the Rectilinear Pitch Cases of AVT-202 (Invited)
Author:
Affiliation:
1. Istanbul Technical University
2. Cambridge University
3. University of Maryland, College Park
4. Air Force Research Laboratory
5. ASELSAN, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0289
Reference25 articles.
1. High-Amplitude Pitch of a Flat Plate: An Abstraction of Perching and Flapping
2. Aerodynamic Performance of a Notional Perching MAV Design
3. Lift and the leading-edge vortex
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