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Internal Ballistics of Hybrid Rocket with a Diaphragm

机译:膜片式混合火箭的内部弹道

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Numerical calculations on the pipe flow with wall blowing was conducted using LES methodology to capture the intrinsic changes of axial small-scale vortices and radial fluctuating motions near the flow surface upon the insertion of diaphragm. The special attentions were devoted to the relation between the flow characteristics of variant turbulent vortices over the diaphragm and the analysis of combustion characteristics by introducing 'Reynolds analogy' theory. Numerical results as well as streak line analysis showed that large-scale vortex over a diaphragm interfered with the existing vortices near the surface. The growth of the small-scale vortices was suppressed until large-scale vortex shed in the downstream pseudo-periodically. In addition, POD (Proper Orthogonal Decomposition) analysis revealed that inserting a diaphragm decreased the energy content in the primary flow mode, and reallocated flow energy in the lower modes 2-5. The increase of flow energy in the lower modes 2-5 was found to be directly associated with the experimentally observed local increase in regression rate after a diaphragm. Finally, the estimation of skin friction coefficient in the flow with a diaphragm showed a very good qualitative agreement with the axial profile of regression rate obtained both by numerical and experimental studies.
机译:使用LES方法对壁吹吹管流动进行了数值计算,以捕获隔膜插入后轴向小尺度旋涡的内在变化以及流表面附近的径向波动运动。通过引入“雷诺类比”理论,特别注意了膜片上不同湍流涡流的流动特性与燃烧特性分析之间的关系。数值结果和条纹线分析表明,膜片上的大规模旋涡干扰了地表附近现有的旋涡。小型涡旋的生长受到抑制,直到大型涡旋在假周期内顺流而下。此外,POD(正确的正交分解)分析表明,插入隔膜会降低一次流动模式下的能量含量,并在较低模式2-5下重新分配流动能。发现在较低模式2-5中流动能量的增加与膜片后通过实验观察到的回归速率的局部增加直接相关。最后,用隔膜进行的流动中皮肤摩擦系数的估计与数值和实验研究得出的回归速率的轴向轮廓显示出非常好的定性一致性。

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