An investigation of the canard aspect ratio and spacing on the aerodynamics of the main wing
Author:
Affiliation:
1. Auburn University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1982
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1. Challenges Facing Future Micro-Air-Vehicle Development
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3. AERODYNAMICS OF SMALL VEHICLES
4. Jung, Y. W., and Park, S. O. "Vortex-shedding characteristics in the wake of an oscillating airfoil at low Reynolds number," Vol.20, 2005, pp.451-464. https://doi.org/10.1016/j.jfluidstructs.2004.11.002.
5. Effects of Pivot Location and Reduced Pitch Rate on Pitching Rectangular Flat Plates
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