Decomposed Lifting-Line Predictions and Optimization for Propulsive Efficiency of Flapping Wings
31st AIAA Applied Aerodynamics Conference
San Diego, CA
American Institute of Aeronautics and Astronautics
A decomposed Fourier series solution to Prandtl's classical lifting-line theory is used to predict the lift, induced-thrust, and power coefficients developed by a flapping wing. A significant advantage of this quasi-steady analytical solution over commonly used numerical methods is the utility provided for optimizing wing flapping cycles. The analytical solution involves five time-dependent functions that could all be optimized to maximize thrust, propulsive efficiency, and/or other performance measures. Results show that by optimizing only two of these five functions, propulsive efficiencies exceeding 97% can be obtained. Results are presented for untwisted rectangular wings in pure plunging, rectangular wings with linear washout and the minimum-power washout magnitude, and rectangular wings with the minimum-power washout distribution and magnitude.
Phillips, W. F., Miller, R. A., Hunsaker, D. F., “Decomposed Lifting-Line Predictions and Optimization for Propulsive Efficiency of Flapping Wings,” 31st AIAA Applied Aerodynamics Conference, San Diego, California, June 24 – 27, 2013, AIAA-2013-2921.
Additional FilesAIAA-2013-2921-Supplemental.pdf (2913 kB)