CFD Simulation Data for Supersonic Flow over an Aircraft Wing
Published: 27 April 2026| Version 1 | DOI: 10.17632/5zwmnnw2b8.1
Contributor:
FAVOUR OJIAKUDescription
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.
Files
Institutions
- Teesside UniversityEngland, Middlesbrough
Categories
Aerodynamics, Computational Fluid Dynamics / Discrete Element Method Model