Experimental and numerical investigation of a supersonic inlet with double S-bend diffuser
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DOI: 10.1177/0954410020983981
Abstract: Design of a supersonic inlet with double S-bend diffuser was developed. Numerical simulation and wind tunnel experiment were carried out to investigate the aerodynamic performance and variable geometric rules of the inlet. The result indicates… read more here.
Keywords: bend; bend diffuser; supersonic inlet; double bend ... See more keywords