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The stagnation point offsets of turbulent opposed jets at various exit velocity ratios and nozzle separations were experimentally studied by a hot-wire anemometer, smoke-wire technique and numerically simulated by Reynolds stress model (RSM). Results show that for 2D≤L≤4D (where L is nozzle separation and D is nozzle diameter), the position of the impingement plane is unstable and oscillates within...
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