Image Gallery

Numerical simulation of an unstart event in the Hypersonic Research Engine configuration carried out using Stanford's computational tools. The time-evolution is left-to-right and top-to-bottom and the snapshots correspond to 1ms.

Hyshot scramjet vehicle developed and launched by University of Queensland (Australia) in 2004. The top figure represents a numerical simulation of the shock wave structure at a flight Mach number of 7.5 and corresponding to an altitude of 27Km



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