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Gas dynamics and flow characteristics of highly turbulent under-expanded hydrogen and methane jets under various nozzle pressure ratios and ambient pressures

机译:在不同的喷嘴压力比和环境压力下,高度湍流的膨胀不足的氢气和甲烷喷嘴的气体动力学和流动特性

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The current study used large eddy simulations to investigate the sonic and mixing characteristics of turbulent under-expanded hydrogen and methane jets with various nozzle pressure ratios issued into various ambient pressures including elevated conditions relevant to applications in direct injection gaseous-fuelled internal combustion engines. Due to the relatively low density of most gaseous fuels such as hydrogen and methane, DI requires high injection pressures to achieve suitable mass flow rates for fast in-cylinder fuel delivery and rapid fuel-air mixing. Such pressures typically form an under-expanded fuel jet past the nozzle exit. Test cases of hydrogen injection with nozzle pressure ratio (NPR) of 10 issued into quiescent air with pressure P-infinity approximate to 1, 5 and 10 bar were simulated. Direct comparison between hydrogen and methane jets with NPR = 8.5 and P-infinity approximate to 1 was also made. The effect of ambient pressure on features of transient development of the near-nozzle shock structure and tip vortices (vortex ring) was investigated. It was observed that at constant NPR, higher ambient pressure resulted in slightly faster formation of the Mach reflection and shorter Mach disk settlement time. Different mechanisms were observed between hydrogen and methane with regards to transient formation of their initial tip vortex rings. It was found that the initial transient tip vortices of hydrogen jets may also contribute to the flow instabilities at the boundary of the intercepting shock and, unlike for methane, promote fuel-air mixing before the Mach reflection. It was also shown that the near-nozzle shock structure was only affected by NPR regardless of the ambient pressure. Furthermore, no flow recirculation zone was found just downstream of the Mach disk, a finding comparable to all previous experimental investigations. Also, it was observed that a locally richer mixture was created for jets with higher NPR or with higher ambient pressure at constant NPR. Based on the results of the current study, correlations were proposed for the shock cell spacing and jet tip penetration of highly under-expanded jets issued from millimetre-size circular nozzles. Copyright (C) 2016, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights reserved.
机译:当前的研究使用大型涡流模拟来研究湍流的膨胀不足的氢气和甲烷射流的声波和混合特性,这些喷嘴具有不同的喷嘴压力比,并产生各种环境压力,包括与直接喷射气态内燃机相关的升高条件。由于大多数气体燃料(例如氢气和甲烷)的密度相对较低,因此DI需要较高的喷射压力才能实现合适的质量流量,以实现缸内燃料的快速输送和燃料与空气的快速混合。这样的压力通常形成经过喷嘴出口的膨胀不足的燃料射流。模拟了在静态压力为P,无穷大,接近1、5和10 bar的静态空气中喷出氢气的喷嘴压力比(NPR)为10的测试案例。还直接比较了NPR = 8.5和P-无穷大接近1的氢气和甲烷喷嘴。研究了环境压力对近喷嘴冲击结构和尖端涡旋(涡环)瞬态发展特征的影响。可以看出,在恒定NPR的情况下,较高的环境压力会导致Mach反射的形成速度稍快,而Mach盘的沉降时间较短。在氢和甲烷之间,关于其初始尖端涡旋环的瞬时形成,观察到不同的机理。已经发现,氢射流的初始瞬态尖端涡流也可能导致拦截激波边界处的流动不稳定性,并且与甲烷不同,它在马赫反射之前促进了燃料与空气的混合。还表明,无论环境压力如何,近喷嘴冲击结构仅受NPR影响。此外,在马赫盘的下游未发现任何流体再循环区,这一发现与之前的所有实验研究都相当。而且,观察到在恒定NPR下,对于具有较高NPR或具有较高环境压力的喷射器,产生了局部较浓的混合物。根据当前研究的结果,提出了与毫米级圆形喷嘴发出的高度未充分膨胀的射流的激波单元间距和射流尖端穿透的相关性。 Hydrogen Energy Publications,LLC(C)2016版权所有。由Elsevier Ltd.出版。保留所有权利。

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