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Investigation of effective liquid fuel mixing technology with low total pressure loss in supersonic flow

机译:超声速总压损失低的有效液体燃料混合技术研究

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The injection and mixing of liquid fuel ejected from alternating wedge strut had been studied. Results show the feature of break up and mixing. However, in order to compare the mixing characteristics of different geometric struts and find the optimal strategy, more works need to be done. Therefore experimental and computational studies of ordinary strut, compression ramp strut and alternating wedge strut have been developed in this paper. The data of flow field structure and total pressure loss will be compared. On this basis, a new strut is designed and some computational works have been finished. In the experiments, schlieren photograph and PLIF are used to take photos. In the computations, fluent software helps researchers to obtain other parameters. The results of this paper indicated that the penetration of three struts had a few differences. But alternating wedge strut and compression ramp strut improved the distribution of fuel. When injected with low pressure, compression ramp strut had the shortest mixing length and the maximum total pressure loss. The improved AW strut promoted mixing and reduced the total pressure loss slightly.
机译:已经研究了从交替楔形支杆喷出的液体燃料的喷射和混合。结果显示了分解和混合的特征。但是,为了比较不同几何支撑的混合特性并找到最佳策略,需要做更多的工作。因此,本文开展了对普通支杆,压缩斜杆支杆和交替楔形支杆的实验和计算研究。将比较流场结构和总压力损失的数据。在此基础上,设计了一个新的支撑杆,并完成了一些计算工作。在实验中,使用schlieren照片和PLIF拍照。在计算中,流畅的软件可帮助研究人员获得其他参数。本文的结果表明,三个支柱的穿透力有一些差异。但是交替的楔形支柱和压缩斜坡支柱改善了燃料的分配。当用低压注入时,压缩坡道支柱具有最短的混合长度和最大的总压力损失。改进的AW支撑杆促进了混合,并略微降低了总压力损失。

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