CFD simulation results on the propeller-induced flow of an octocopter-UAV in hover
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资源简介：
The dataset consists of CFD simulation results on the propeller-induced flow of an octocopter UAV in hover. 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. <br> 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. <br> <br> <br> <br>
创建时间：
2023-05-23
