Abstract
Scientists have long used the unsteady vortex lattice method (UVLM) to simulate flapping-wing flight. However, there are few open-source UVLM solvers designed for research in this field. The newly released Ptera Software is, to the best of the authors’ knowledge, the only open-source UVLM solver for flapping wings that is in active development. This report documents the next steps in Ptera Software’s progress: the validation of its results and the optimization of its performance. Comparing Ptera Software’s output to high-fidelity experimental data of the pressures on a flapping-wing robot shows that the simulated results predict the trends and magnitudes of the net lift over time with reasonable accuracy. Also, by using several computational methods, the researchers optimized the source code such that the solver’s latest iteration is over three times faster than previous versions. The present results demonstrate that Ptera Software correctly implements the UVLM and can simulate flapping-wing flight with reasonable accuracy under this method’s assumptions. Additionally, it is now fast enough for use as an iterative tool in the design of novel flapping-wing micro aerial vehicles (FWMAVs).
Document Type
Final Report
Class Name
Mechanical Engineering and Material Sciences Independent Study
Date of Submission
5-13-2021
Recommended Citation
Urban, Cameron and Agarwal, Ramesh K., "Validation and Optimization of Ptera Software: An Open-Source Unsteady Simulator for Flapping Wings" (2021). Mechanical Engineering and Materials Science Independent Study. 149.
https://openscholarship.wustl.edu/mems500/149