What is it about?
Understanding shock wave interference patterns in nonequilibrium flows is key in the design of hypersonic flight vehicles. Most of the studies of this type of phenomena are limited to canonical 2D geometries. This work presents a numerical study applied to a conceptual 3D wing-body vehicle.
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This page is a summary of: Parametric Study of Nonequilibrium Shock Interference Patterns over a Fuselage-and-Wing Conceptual Vehicle, AIAA Journal, December 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060470.
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