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Scale effect of spherical projectiles for stabilization of oblique detonation waves

机译:球形弹丸对倾斜​​爆轰波稳定的尺度效应

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Oblique detonation waves (ODWs) were stabilized by launching a spherical projectile with 1.2-1.4 times the Chapman-Jouguet (C-J) velocity into detonable mixtures at rest. We used smaller projectiles (3.18 mm diameter) than those (4.76 mm diameter) in our previous studies and investigated the effect of the projectile scale on the stabilization of ODWs. We carried out high time resolution schlieren visualization using a high-speed camera. The detonable mixtures used were stoichiometric oxygen mixtures with acetylene, ethylene or hydrogen. They were diluted with argon with a 50 % volumetric fraction, and a dilute mixture containing 75 % argon was also tested for the acetylene/oxygen mixture. Here, we discuss the detonation stability in terms of the curvature effect arising from the three-dimensional nature of a stabilized ODW around a projectile. The curvature effect attenuated the detonation wave to below its C-J velocity in the vicinity of the projectile before the wave velocity asymptotically reached the C-J velocity in the far field. Our previous study showed that the propagation limit of the curvature effect is responsible for the stabilizing criticality of detonation waves. By obtaining detailed distributions of the wave propagation velocity and radius of curvature at the stabilizing criticality, we showed that the radius of curvature at the local minimum point of the wave propagation velocity represents the critical radius of curvature required for curved self-sustained detonation. In this study, we focused on this critical mode of the stabilized ODW for a small projectile (3.18 mm diameter). Distributions of the wave velocity and radius of curvature were obtained in the critical mode of the stabilized ODW. We compare these distributions with those for a larger projectile (4.76 mm diameter) and discuss the stabilizing criticality. For the small projectile, the observed combustion regimes had qualitatively the same trend for the initial pressure of the mixture as that observed for the large projectile. However, the initial pressure for each combustion regime was quantitatively different for the different projectile scales. The small projectile required a higher initial pressure to stabilize the ODW than the large projectile. For the critical mode of the stabilized ODW, the wave velocity distribution had a local minimum value (0.8-0.9 times the C-J velocity) due to the curvature effect. The radius of curvature at this characteristic point was about five times the projectile radius, regardless of the mixture composition. The radius of curvature normalized by the cell size was about 8-10 and 15 for mixtures diluted with 50 and 75 % argon, respectively, regardless of the projectile diameter. These results mean that the projectile radius (diameter) proportionally affects the geometrical scale of the wave around the projectile, and the fraction of the gas used for dilution affects the cell size required to sustain a curved detonation wave. The stabilizing criticality, expressed as the dimensionless projectile diameter (projectile diameter normalized by cell size), was about 3.5 and 5.5 for mixtures diluted with 50 and 75 % argon, respectively. These criticalities agreed with those of the large projectile of the previous study. This indicates that the dimensionless projectile diameter is a unique parameter for the stabilizing criticality regardless of the projectile diameter.
机译:倾斜的爆轰波(ODW)通过以1.2到1.4倍的查普曼-乔格(C-J)速度发射球形弹丸到静止的可爆炸混合物中来稳定。在我们先前的研究中,我们使用的弹丸(直径为3.18 mm)比弹药(直径为4.76 mm)更小,并研究了弹丸规模对ODW稳定性的影响。我们使用高速摄像头进行了高分辨率的schlieren可视化。所使用的可爆炸混合物是与乙炔,乙烯或氢的化学计量的氧气混合物。将它们用体积分数为50%的氩气稀释,并测试含75%氩气的稀混合物的乙炔/氧气混合物。在这里,我们将从弹丸周围​​的稳定ODW的三维性质引起的曲率效应方面讨论爆轰稳定性。在波速渐近地达到远场中的C-J速度之前,曲率效应使爆炸波在弹丸附近衰减至其C-J速度以下。我们以前的研究表明,曲率效应的传播极限是引起爆轰波稳定的关键。通过获得稳定临界点处波传播速度和曲率半径的详细分布,我们证明了波传播速度的局部最小值处的曲率半径代表了弯曲自持爆轰所需的临界曲率半径。在这项研究中,我们将重点放在小弹丸(直径3.18毫米)的稳定ODW的临界模式上。在稳定的ODW的临界模式下获得了波速和曲率半径的分布。我们将这些分布与较大的弹丸(直径为4.76 mm)进行比较,并讨论了稳定度的重要性。对于小弹丸,混合物的初始压力所观察到的燃烧方式在质量上与大弹丸具有相同的趋势。但是,对于每种燃烧状态,初始压力在不同的射弹比例上在数量上是不同的。小弹丸比大弹丸需要更高的初始压力才能稳定ODW。对于稳定的ODW的临界模式,由于曲率效应,波速分布具有局部最小值(C-J速度的0.8-0.9倍)。无论混合物成分如何,在此特征点处的曲率半径约为弹丸半径的五倍。不管弹丸直径如何,用50%和75%的氩气稀释的混合物的泡孔大小归一化的曲率半径分别约为8-10和15。这些结果意味着,弹丸半径(直径)成比例地影响弹丸周围波的几何尺度,而用于稀释的气体比例会影响维持弯曲爆轰波所需的像元大小。对于用50%和75%氩气稀释的混合物,稳定临界值分别表示为无因次射弹直径(通过泡孔尺寸归一化的射弹直径),分别约为3.5和5.5。这些临界与先前研究的大型弹丸相一致。这表明无量纲弹丸直径是稳定临界值的唯一参数,与弹丸直径无关。

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