Experimental investigation of nose-tip temperature effects on the hypersonic crossflow instability over a yawed cone at Mach 6
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DOI: 10.1063/5.0248996
Abstract: In this paper, the influence of the nose-tip temperature on hypersonic crossflow instability is experimentally investigated using infrared thermal imaging and high-frequency pulsating pressure sensors at Mach 6 for a 7° semi-cone angle of 6°… read more here.
Keywords: temperature; tip temperature; hypersonic crossflow; crossflow instability ... See more keywords