CFD Simulation Data for Supersonic Flow over an Aircraft Wing

Published: 27 April 2026| Version 1 | DOI: 10.17632/5zwmnnw2b8.1
Contributor:
FAVOUR OJIAKU

Description

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

Categories

Aerodynamics, Computational Fluid Dynamics / Discrete Element Method Model

Licence