Measurements of thermal effects on acoustic screech in a choked circular jet emanating from a sharp-edged orifice

【Author】

Max Kandula;

【Abstract】

<正>Experiments are performed in a 24.4 mm diameter choked circular jets(hot and cold) issuing from a sharp-edge orifice at a fully expanded jet Mach number of 1.85.The stagnation temperature of the hot and the cold jets are 319 K and 299 K,respectively.The

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