Fábio Henrique Eugênio Ribeiro, André Carlos Fraile Júnior

DOI Number XXX-YYY-ZZZ

Conference Number HiSST-2022-389

Scramjet engines are high-speed airbreathing propulsion systems with no moving parts, which compress the air dynamically through a supersonic intake, increasing temperature and pressure levels so
combustion can occur. Flow dynamics in a generic scramjet combustion chamber is studied based on a
representative experiment run at the Institute for Advanced Studies. The computations are performed
with an in-house solver that is being developed to perform simulations of compressible reactive multicomponent flows. The present simulations are performed within the LES framework and WALE model
is retained as the SGS viscosity closure, and the geometry of the combustor is modeled using the IBM
algorithm.

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In Categories: 1.Events, HiSST 2022, Testing and Evaluation
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