CFD simulation results on the propeller-induced flow of an octocopter-UAV in hover

<p>The dataset consists of CFD simulation results on the propeller-induced flow of an octocopter UAV in hover. </p> <p>The simulations are obtained using RANS, the k − ε turbulence model, and the actuator disc theory. System geometry, mesh construction, and calculations were done using the commercial software Ansys Fluent 2022 R1.</p> <p><br></p> <p>Further details on the geometry design (e.g. computational domain, UAV architecture, boundary conditions), mesh construction,  calculations setup, and reading of the dataset can be found in the ReadMe file.</p> <p><br></p> <p><br></p> <p><br></p> <p><br></p>