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

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>

本数据集涵盖某八旋翼无人机（octocopter UAV）悬停工况下螺旋桨诱导流的计算流体动力学（Computational Fluid Dynamics, CFD）仿真结果。本次仿真依托雷诺平均纳维-斯托克斯（Reynolds-Averaged Navier-Stokes, RANS）方程、k−ε湍流模型与致动盘理论完成，系统几何建模、网格构建与仿真计算均通过商用软件Ansys Fluent 2022 R1实现。

有关几何设计（如计算域、无人机架构、边界条件）、网格构建、计算设置以及数据集读取方式的更多细节，请参阅ReadMe文件。