Purpose - Test the aerodynamic analysis code VSPAERO, which is part of OpenVSP from NASA. Apply VSPAERO to calculate the lift curve slope and the span efficiency factor of straight wings (for various
ASCII file containing aerodynamic forces around an A320 wing. From a 2D numerical simulation performed with the NSMB code. The first four columns give the physical time in seconds, the drag coefficien
These are data and JAGS model files for Skandalis et al. 2017, The biomechanical origin of extreme wing allometry in hummingbirds For descriptions of the data, see README analysis_data_power.txt, and
Data for "Behavior and Biomechanics: Flapping frequency during tandem and solo flights of Cliff Swallows" Data for this project are provided as a single Zip archive with a hierarchical folder s
Mass in gram, fiber lengths in mm. N = 1 for all species except G. fortis where N = 4. For the smaller species C. olivacea, C. parvulus and G. fuliginosa the distinction between the medial and lateral