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Velocity behavior downstream of perforated plates with large blockage ratio for unstable and stable detonations

机译:大阻塞率的多孔板下游的速度行为,用于不稳定和稳定的爆炸

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Due to the excellent thermal propulsion performances of detonation, it has been applied for the purpose of aerospace propulsion devices, e.g., pulse detonation engines (PDEs), rotating detonation engines (RDEs), and oblique detonation wave engines (ODWEs). However, it remains challenging for developing those new-concept propulsion devices, mainly because it is a formidable task to establish a steady and self sustained detonation in the hypersonic flow and combustible mixture. One of the fundamental problems is to understand the interaction of diffractions and the detonation waves within the engines. In this study, perforated plates with various blockage ratios are seated at the beginning of the detonation propagation to explore the diffractions that generated from the plates on the detonation propagation mechanism. Two explosive mixtures of C2H2 + 5N(2)O and C2H2 + 2.5O(2) + 70% Ar are studied to illustrate the difference in propagation velocity behavior of detonation after it suffers from large-scale diffractions. The results show that diffractions have less effect on the propagation of highly unstable mixture, and the effect becomes obvious as BR increases to 0.962; this phenomenon occurs because detonation has an irregular cellular pattern and sub-structures are characterized by highly unstable detonation, in which the detonation instabilities are amplified by the large perturbations of obstacles, leading to an augment in forming more cellular cells of detonation in its front that cover the weakening effects from diffractions. In contrast, the diffractions significantly affect the stable mixture, manifested by a remarkable increase of the critical pressure for a self-sustained detonation downstream of the obstacle with the augment of blockage ratio: this phenomenon can be attributed to the diffractions being distributed along the curvature over the detonation surface, thereby causing more excessive curvature of the entire detonation front, which in turn exacerbates the failure of detonation. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:由于起爆具有出色的热推进性能,因此已被用于航空航天推进装置,例如脉冲起爆发动机(PDE),旋转起爆发动机(RDE)和倾斜起爆波发动机(ODWE)。但是,开发这些新概念的推进装置仍然具有挑战性,主要是因为在高超音速流和可燃混合物中建立稳定且自持的爆炸是一项艰巨的任务。基本问题之一是要了解发动机内部的衍射和爆炸波的相互作用。在这项研究中,将具有各种阻塞率的多孔板放置在爆炸传播的开始处,以探讨由板在爆炸传播机理上产生的衍射。研究了C2H2 + 5N(2)O和C2H2 + 2.5O(2)+ 70%Ar的两种爆炸性混合物,以说明爆炸受到大规模衍射后,其传播速度行为的差异。结果表明,衍射对高度不稳定混合物的传播影响较小,当BR增加至0.962时,这种影响变得明显。发生这种现象是因为爆炸具有不规则的细胞模式,并且子结构的特征是高度不稳定的爆炸,其中较大的障碍物扰动会放大爆炸的不稳定性,从而导致在其前面形成更多的爆炸细胞而导致爆炸。涵盖了衍射的减弱作用。相比之下,衍射显着影响稳定的混合物,表现为障碍物下游自持爆轰的临界压力显着增加,且阻塞率增大:这种现象可归因于衍射沿着曲率分布爆轰表面上的爆轰,从而导致整个爆轰锋面弯曲更大,从而加剧了爆轰的失败。 (C)2019 Elsevier Masson SAS。版权所有。

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