Numerical evaluation of effects of the isolator height and the leading-edge bluntness on a scramjet inlet
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DOI: 10.1007/s40430-020-02352-z
Abstract: Air-breathing hypersonic vehicles can be powered by scramjet (supersonic combustion ramjet) engines, whose inlet requires blunt leading edges in order to overcome the high heat fluxes that are inherent of hypersonic flights. Thus, this work… read more here.
Keywords: isolator height; edge bluntness; isolator; leading edge ... See more keywords