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Computational and Experimental Investigation of Inclined Choked Injection of Gaseous Jet

机译:斜向注入气态射流的计算和实验研究

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The injection of choked gaseous jets into still air is investigated computationally and experimentally. The objective is to compare the performance of three turbulence models -Realizable k-ε, SST k-ω and Reynolds Stress Transport to resolve 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 that has been seeded with water fog. The test conditions include injection angles of 0° and 15°. The results including jet velocities and the vorticity field 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:通过计算和实验研究了将窒息的气态射流注入静止空气的过程。目的是比较三种湍流模型的性能-可实现的k-ε,SSTk-ω和雷诺应力传递,以解决喷射角度对与环境空气混合射流的影响。实验方法由粒子图像测速法(PIV)组成,该粒子测速(PIV)使用阻塞气体射流的脉冲Nd:YAG激光器注入氧化铝颗粒,注入已注入水雾的静止空气中。测试条件包括0°和15°的喷射角。给出了包括射流速度和涡度场在内的结果。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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