03.1 - Aerodynamics – CFD Methods and Validation
DETACHED EDDY SIMULATION OF HYPERSONIC SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE-CYLINDER-FLARE
R.O. Bura, Republic Indonesia Defense University, Indonesia; A. Riyadl, National Research and Innovation Agency, Indonesia
In the 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 were analyzed. Detached Eddy Simulation (DES) and k-? turbulence models were used and the simulation results were compared to the experimental result of HIFiRE-1 ground test studies.