Effect of shock generator on fuel mixing in an annular single lobe transverse nozzle at the supersonic combustion chamber of a scramjet engine using computational fluid dynamics

Evaluation of Influences of Changed Lower Cover Geometry on Kerosene–Air Interaction in a Scramjet Combustor

“…Although the flow topologies in the scramjet combustor have been the subjects of extensive experimental and numerical work, , the adverse effects of the supersonic air on the scramjet combustor have not been considered in any detail. In the scramjet combustor, the supersonic air is generally produced by the lower cover, as schematically indicated by number 7 in Figure B.…”