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Published in 2017 at "Journal of Propulsion and Power"
DOI: 10.2514/1.b36414
Abstract: Vortex generators within a two-dimensional external-compression supersonic inlet for Mach 1.6 were investigated to determine their ability to increase total-pressure recovery, reduce total-pressure distortion, and improve the boundary layer. The vortex generators studied included vanes…
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Keywords:
dimensional external;
inlet;
compression supersonic;
two dimensional ... See more keywords