Optimizing the Forces and Propulsive Efficiency in Bird-Scale Flapping Flight
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4916
Reference14 articles.
1. Neurobiologically Inspired Control of Engineered Flapping Flight
2. Recent progress in flapping wing aerodynamics and aeroelasticity
3. Dynamics, stability, and control analyses of flapping wing micro-air vehicles
4. A Flight Mechanics-Centric Review of Bird-Scale Flapping Flight
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1. Periodic Optimal Control for Reducing the Fuel Consumption of Flapping Wing Vehicles;AIAA SCITECH 2023 Forum;2023-01-19
2. Approximate Model for Cycle-Averaged Aerodynamic Forces, and its Application to Stability and Control of Bird-Scale Flapping-Wing Aircraft;AIAA Scitech 2020 Forum;2020-01-05
3. Optimization of the Spanwise Twist of a Flapping Wing for Bird-sized Aircraft using a Quasi-Steady Aerodynamic Model;International Journal of Aeronautical and Space Sciences;2019-03-06
4. Closed-Form Expressions for Cycle-Averaged Aerodynamic Quantities at an Airfoil Section of an Avian Flapping Wing;AIAA Scitech 2019 Forum;2019-01-06
5. Performance Analysis of a Self-Propelling Flat Plate Fin with Joint Compliance;Journal of The Institution of Engineers (India): Series C;2017-12-04
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