Thermofluidic compression effects to achieve combustion in a low-compression scramjet engine
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DOI: 10.1007/s00193-017-0782-0
Abstract: The compression provided by a scramjet inlet is an important parameter in its design. It must be low enough to limit thermal and structural loads and stagnation pressure losses, but high enough to provide the… read more here.
Keywords: compression; equivalence; engine; combustion ... See more keywords