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Numerical investigation of flow instability in shock tube due to shock wave-contact surface interactions

机译:冲击波与接触面相互作用引起的激波管流动不稳定性的数值研究

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Purpose - The purpose of this paper is to perform a computational fluid dynamics (CFD) simulation that is able to reveal what is happening for the shock wave generated by high speed flow test facility and to develop deeper understanding of all parameters which affect the shock wave velocity profile and pressure and temperature histories inside the facility. Design/methodology/approach - Two dimensional time accurate Euler solver for shock tube applications was developed to simulate the flow process inside the shock tube. To ensure the ability of the CFD code to capture shocks, rarefaction waves and contact discontinuity and to produce the correct pressure, temperature, density and speed profiles, the code has been validated using two verification approaches. First, the code results have been compared to the Sod's tube problem (exact solution). Second, the code solution is compared with selected experimental measurements for a certain diaphragm pressure ratio. Findings - Results presented in this paper show that after diaphragm rapture and when the shock did not reflect yet, the flow is symmetry and uniform in y-direction. As the shock wave reflects from the tube end it will move to the left and interact with the discontinuity surface and the flow no longer symmetry. Results also show that two-dimensional modeling of the high speed flow test facility is an effective way to obtain facility performance data. Although this paper focused on UNITEN's facility, the CFD code is generic and may be applied to other facilities. The present code showed good capability to provide the x-t diagram successfully. From this diagram one can determine the useful duration (for this case it is about 10 ms), which is quite comparable compared to other facilities. It can be concluded, based on the agreement with the analytical results, that the numerical formulation for the inviscid part of the solver is valid. Originality/value - This paper performs a CFD simulation that is able to reveal the shock wave behavior at high speed flow test facility.
机译:目的-本文的目的是进行计算流体动力学(CFD)仿真,该仿真能够揭示高速流量测试设备所产生的冲击波的情况,并加深对影响冲击波的所有参数的了解设备内部的速度曲线以及压力和温度历史记录。设计/方法/方法-开发了适用于冲击管的二维时间精确的Euler求解器,以模拟冲击管内部的流动过程。为了确保CFD代码能够捕获冲击,稀疏波和接触不连续并产生正确的压力,温度,密度和速度曲线,已使用两种验证方法对代码进行了验证。首先,将代码结果与Sod's tube问题(精确解决方案)进行了比较。其次,将代码解决方案与选定的实验测量结果进行比较,以得出一定的隔膜压力比。研究结果-本文提出的结果表明,在膜片破裂后并且当冲击还没有反映出来时,流动在y方向上是对称且均匀的。当冲击波从管端反射时,它将向左移动并与不连续面相互作用,并且流动不再对称。结果还表明,对高速流动测试设施进行二维建模是获得设施性能数据的有效方法。尽管本文着重介绍UNITEN的设施,但CFD代码是通用的,可以应用于其他设施。当前代码显示了成功提供x-t图的良好能力。从该图可以确定有用的持续时间(在这种情况下约为10毫秒),与其他设施相比相当。根据与分析结果的一致性可以得出结论,求解器无粘性部分的数值公式是有效的。原创性/价值-本文进行了CFD仿真,能够揭示高速流量测试设备中的冲击波行为。

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