M. R.

Comparative CFD Analysis of SST k–ω and Spalart–Allmaras Turbulence Models for Aerodynamic Force Prediction of a Grid-Fin Missile at Mach 2.5 and 10° Angle of Attack

The aerodynamic performance of aerospace vehicles operating in supersonic flow regimes is significantly influenced by the accurate prediction of complex flow phenomena, flow separation and turbulent boundary-layer interactions. The present study investigates the aerodynamic characteristics of the selected configuration...