Supplementary animations and simulation settings for "Wake Aerodynamic of Multi-Rotor System with Lifting-Devices Under Different Ambient Turbulence"

################################Animations, case setting and source code for "Wake Aerodynamic of Multi-Rotor System with Lifting-Devices Under Different Ambient Turbulence".<br>################################Educational and research use of the material is permitted. Please cite the following reference when using/expanding the code, graphics and data:<br>Y. Li, W. Yu, A. Sciacchitano, C. Ferreira, 2025 Wake Aerodynamic of Multi-Rotor System with Lifting-Devices Under Different Ambient Turbulence, Journal of Physics: Conference Series (Wake conference 2025).<br>################################<br>The simulations were performed using OpenFOAM v2312https://www.openfoam.com, OpenCFD Ltd<br>################################ANIMATIONS<br>Stored in directory "animations".<br>Animation for cases UW-53, WL-53, and DW-53 are provided. The arrows are scaled by the square root of the instantaneous in-plane velocity's norm.<br>################################<br>CASE SETTINGS<br>Stored in directory "caseSettings".<br>All of the cases settings appeared in the manuscript can be found. Every case used 108 processor sand ran for around 100 hr to complete. We performed the computation on "National Supercomputer Snellius" (Netherland). Job script used by the author is provided ("fullrunDiskActuator.sh"). Mesh can be generated by executing the commands in the job script. Before running the case, please set the path (&lt;yourPath&gt;) in controlDict to include the required module. Note that the mesh for laminar inflow cases were different form the turbulent inflow cases (we did not execute application snappyHexMesh when running cases with laminar inflow). Note that the cases were set mostly through modifying file "parameterMaster". Note that some of the parameters are actually useless, they are there for "historical reasons".<br><br>################################SOURCE CDOE<br>Stored in directory "caseSettings/src".<br>Source code for the library used is provided in directory "src". Execute "Allwmake" and the library should be compiled automatically (file "libflyingActuatorDisk.so" should be generated somewhere depend on how the path is set). If it gives errors, one may have to check the path setting that depends on the machine one uses (in the file "src/Make/files"). Note that in the source code, many lines/variables are not used, they are there for "historical reasons".<br>################################<br>

################################本数据集包含《不同环境湍流下带升力装置的多旋翼系统尾流气动特性》相关动画、案例设置与源代码。
################################本材料可用于教学与研究用途。在使用、拓展该代码、图表及数据时，请引用如下文献：
Y. Li, W. Yu, A. Sciacchitano, C. Ferreira, 2025 不同环境湍流下带升力装置的多旋翼系统尾流气动特性, Journal of Physics: Conference Series (Wake conference 2025).
################################本仿真基于OpenFOAM v2312（https://www.openfoam.com）完成，开发方为OpenCFD Ltd。
################################动画
动画存储于"animations"目录。本次提供了UW-53、WL-53及DW-53三个案例的动画。动画中箭头的缩放比例由瞬时面内速度模长的平方根决定。
################################案例设置
案例设置文件存储于"caseSettings"目录。论文中出现的所有案例设置均可在此处获取。每个案例均采用108个处理器核心进行计算，总运行时长约100小时。本计算工作在荷兰国家超级计算机Snellius上完成。作者使用的作业脚本已提供（"fullrunDiskActuator.sh"）。网格可通过执行作业脚本中的命令生成。运行案例前，请将"controlDict"中的路径（<yourPath>）配置为包含所需依赖模块。需注意，层流入流案例的网格与湍流入流案例的网格存在差异——层流入流案例无需执行"snappyHexMesh"应用。本案例大多通过修改"parameterMaster"文件进行配置。部分参数实际未被使用，仅因“历史遗留原因”保留。
################################源代码
源代码存储于"caseSettings/src"目录。所用库的源代码位于"src"子目录中。执行"Allwmake"命令即可自动编译该库（根据路径配置的不同，最终将生成"libflyingActuatorDisk.so"文件）。若编译报错，需检查依赖于运行环境的路径配置（修改"src/Make/files"文件）。需注意，源代码中存在大量未使用的行与变量，仅因“历史遗留原因”保留。
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