Reflected shock tube experiments on aeroacoustic signature of hot jets
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DOI: 10.1007/s12206-017-0725-9
Abstract: We used a reflected shock tube to investigate the acoustic signature of a hot jet at the far-field. Experiments were performed at Mach = 1.4 and a total temperature of Tt = 950 Kelvin. Far-field… read more here.
Keywords: signature hot; reflected shock; jet; shock tube ... See more keywords