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Published in 2017 at "Journal of Propulsion and Power"
DOI: 10.2514/1.b36434
Abstract: The influences of inlet geometry modification on flow and combustion dynamics are experimentally investigated in a model supersonic combustion ramjet (scramjet) installed in Mach 4.5 high-enthalpy air freestreams. The inlet upper-lip angle (6, 12, and…
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Keywords:
inlet geometry;
influences inlet;
combustion dynamics;
combustion ... See more keywords