Skip to main content
Other
Decomposed Lifting-Line Predictions and Optimization for Propulsive Efficiency of Flapping Wings
31st AIAA Applied Aerodynamics Conference
  • W. F. Phillips, Utah State University
  • R. A. Miller, Utah State University
  • Doug F. Hunsaker, Utah State University
Document Type
Conference Paper
Publisher
American Institute of Aeronautics and Astronautics
Publication Date
6-24-2013
Abstract
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.
Citation Information
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.