  This article reports on a full replication study in computational fluid
dynamics, using an immersed boundary method to obtain the flow around a
pitching and rolling elliptical wing. As in the original study, the
computational experiments investigate the wake topology and aerodynamic forces,
looking at the effect of: Reynolds number (100--400), Strouhal number
(0.4--1.2), aspect ratio, and rolling/pitching phase difference. We also
include a grid-independence study (from 5 to 72 million grid cells). The trends
in aerodynamic performance and the characteristics of the wake topology were
replicated, despite some differences in results. We declare the replication
successful, and make fully available all the digital artifacts and workflow
definitions, including software build recipes and container images, as well as
secondary data and post-processing code. Run times for each computational
experiment were between 8.1 and 13.8 hours to complete 5 flapping cycles, using
two compute nodes with dual 20-core 3.7GHz Intel Xeon Gold 6148 CPUs and two
NVIDIA V100 GPU devices each.
