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首页> 外文期刊>Journal of Spacecraft and Rockets >Unsteady Supersonic Flows over a Backward-Facing Step with Applied Magnetic Field
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Unsteady Supersonic Flows over a Backward-Facing Step with Applied Magnetic Field

机译:在施加磁场的情况下,超音速流向后倾斜

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Time-dependent behavior of shock/boundary-layer interaction has been investigated numerically for flows over anbackward-facing step. Using a multiblock-grid strategy, the global domain of computation has been decomposed intontwo subdomains representing upstream and downstream regions from the step location. First, Navier–Stokesnanalysis has been performed to investigate the unsteady shock/boundary-layer interaction. Subsequently, magnetofluid-ndynamics computations have been performed to explore the effects of applied magnetic field over the unsteadynnature of the problem and its use for local flow control. A time-explicit modified Runge–Kutta scheme with totalvariation-ndiminishing limiters under a multiblock-grid approach has been implemented. The governing equationsnare composed of the Navier–Stokes equation modified to include the effect of magnetic field under low-magnetic-nReynolds-number approximation. The effects of an applied magnetic field and a time-dependent magnetic field onnthe flowfield have been investigated. It has been shown that the application of magnetic field increases the unsteadynnature of the problem.
机译:冲击/边界层相互作用的时间相关行为已经在数值上研究了朝后步骤的流动。使用多块网格策略,已将计算的全局域分解为代表步位置上游和下游区域的两个子域。首先,已经进行了Navier–Stokesnanalysis,以研究不稳定的冲击/边界层相互作用。随后,进行了磁流体-动力学计算,以探讨施加磁场对问题非定常性的影响及其在局部流动控制中的应用。在多块网格方法下,已实现了具有时间变化的改进Runge-Kutta方案,该方案具有减少总变化量的限制器。控制方程由Navier-Stokes方程组成,该方程经过修改以包含低磁nReynolds数近似下的磁场影响。研究了外加磁场和随时间变化的磁场对流场的影响。已经表明,磁场的施加增加了问题的不稳定性。

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