33th Congress of the International Council of the Aeronautical Sciences

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.


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