Host: The Japan Society of Mechanical Engineers
Name : [in Japanese]
Date : October 18, 2024 - October 20, 2024
In this paper, hypersonic flow around flight test model is simulated using scFLOW, which is a comprehensive computational fluid dynamics (CFD) simulation package designed to handle complex geometries with unstructured grids consisting of arbitrary polyhedral cells. The heat flux is simulated and evaluated using laminar and several Reynolds Averaged Navier-Stokes (RANS) models. The validity of this comprehensive simulation package is shown in comparison with previous experimental data.