Inclined Injection of Under Expanded Supersonic Gas Jet

A. Sheridan, S. Srivastava, M. Henneke, M. S. Raza, K. Sallam
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引用次数: 1

Abstract

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.
欠膨胀超音速气体射流的倾斜喷射
在许多工业应用中,包括火炬和燃烧器,对向静止空气中喷射窒息气体射流进行了实验研究。目的是研究喷射角对射流与周围空气混合的影响。实验方法包括粒子图像测速(PIV),使用脉冲Nd:YAG激光器的窒息气体射流,播种氧化铝颗粒,注入静止空气,播种水雾。计算方法包括使用Star CCM+模拟770万个细胞。测试条件包括注入角为0°、15°和30°。给出了平均速度、脉动速度和流动涡度的计算结果。射流出口膨胀风扇的不对称触发是由于射流平面倾斜造成的,流场沿喷射轴方向不对称。此外,数值模拟还揭示了喷射口内膨胀风机与激波复杂的相互作用机理。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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