03.1 - Aerodynamics – CFD Methods and Validation
TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE IN HYPERSONIC FLOWS
R.O. Bura, Republic of Indonesia Defense University, Indonesia; F.A. Maulana, Indonesia
In this present work, the turbulent Shock-Wave/Boundary-Layer Interactions (SWBLIs) over a geometry model of HIFiRE-1 axisymmetric cone cylinder flare with a ramp angle of 7 and 33 degrees at Mach 7.16 were analyzed.Validation and analysis of turbulence modeling were compared to the experimental result for HIFiRE-1 ground test studies.