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INCLINED INJECTION OF UNDER EXPANDED SUPERSONIC GAS JET

机译:膨胀超音速射流的斜射

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The injection of choked gaseous jets into the still air is investigated experimentally motivated by many industrial applications including flares and burners. The objective is to study the effect of injection angle on the jet mixing with ambient air. The experimental methods consist of particle image velocimetry (PIV) using pulsed Nd.YAG lasers of a choked gas jet, seeded with aluminum oxide particles, injected into still air, seeded with water fog. The computational methods consisted of 7.7 million cells simulation using Star CCM+. The test conditions include injection angles of 0°, 15°, and 30°. The results including mean and fluctuating velocities and the flow vorticity are presented. The flow field is not symmetric along the injection axis due to the asymmetric triggering of expansion fans at the jet exit due to the inclined injection plane. Moreover, the numerical simulation reveals the complex interaction mechanism of the expansion fans and Shockwaves within the injection port.
机译:在许多工业应用(包括火炬和燃烧器)的驱动下,对of气喷射到静止空气中进行了实验研究。目的是研究喷射角度对与环境空气混合射流的影响。实验方法包括使用using流气体脉冲Nd.YAG脉冲激光的粒子图像测速(PIV),该粒子用氧化铝粒子播种,注入到静止的空气中,水雾播种。计算方法包括使用Star CCM +进行的770万个细胞模拟。测试条件包括0°,15°和30°的喷射角。给出了包括平均速度和波动速度以及流动涡度在内的结果。由于倾斜的喷射平面,由于射流出口处膨胀风扇的不对称触发,流场沿喷射轴不对称。此外,数值模拟揭示了进样口内膨胀风扇和激波的复杂相互作用机理。

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