CFD Simulation Data for Supersonic Flow over an Aircraft Wing
收藏DataCite Commons2026-04-27 更新2026-05-04 收录
下载链接：
https://data.mendeley.com/datasets/5zwmnnw2b8
下载链接
链接失效反馈官方服务：
资源简介：
Dataset containing CFD simulation inputs and outputs for supersonic flow analysis over an aircraft wing, including mesh data, boundary conditions, pressure and Mach distributions, shock-wave results, and aerodynamic performance outputs.
提供机构：
Mendeley Data
创建时间：
2026-04-27
