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Stability of boundary layers within high-speed viscous flows.

机译:高速粘性流中边界层的稳定性。

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A numerical study was undertaken to predict the stability of a variety of high-speed boundary-layer flows. Using a finite-volume code, the Navier-Stokes equations were solved for a series of flows around spherically blunted cones. These solutions were used to perform linear-stability analyses for second-mode disturbances.; Two investigations were undertaken using an ideal-gas model: the Stetson experiment and a recent experiment conducted at the Institute of Theoretical and Applied Mechanics in Russia. Comparisons were made with both basic-state and disturbance state quantities. For both cases, linear-growth regions have been identified. For the Stetson case, using an experimentally determined wall-temperature distribution for the basic-state appeared to give better agreement with the experimentally measured growth than does the classical adiabatic-wall boundary condition. For the Russian experiment, initial comparisons were made in order to continue a careful collaboration.; A third investigation was made which used a chemical non-equilibrium model, considering a Mach 13.5 flow in upper-atmospheric conditions. The goal of this investigation was to evaluate the sensitivity of second-mode growth predictions to changes (within accepted uncertainties) in thermodynamic, reaction-rate; and transport models. The magnitude of change in the stability results correlated strongly with changes in the basic-state thermal boundary-layer profile, consistent with second-mode theory. The largest change in the stability behavior was observed for the case where the transport model was changed.; For high-speed flows, the development of computational techniques is in some ways ahead of the experimental community's ability to verify the results. As these techniques are applied to flows in thermochemical non-equilibrium, the fidelity of the constitutive relationships should be considered.
机译:进行了数值研究,以预测各种高速边界层流的稳定性。使用有限体积代码,求解了围绕球形钝锥的一系列流动的Navier-Stokes方程。这些解决方案用于对第二模式干扰进行线性稳定性分析。使用理想气体模型进行了两项研究:Stetson实验和最近在俄罗斯理论与应用力学研究所进行的实验。比较了基本状态量和干扰状态量。对于这两种情况,已经确定了线性增长区域。对于Stetson案例,与经典的绝热壁边界条件相比,使用实验确定的基态壁温分布似乎与实验测量的增长更好地吻合。对于俄罗斯实验,进行了初步比较,以继续进行仔细的合作。考虑到高气压条件下的马赫数为13.5,使用化学非平衡模型进行了第三次调查。这项研究的目的是评估第二模式增长预测对热力学反应速率变化(在可接受的不确定性范围内)的敏感性。和运输模型。稳定性结果的变化幅度与基本态热边界层分布的变化密切相关,这与第二模态理论一致。在运输模型改变的情况下,观察到稳定性行为的最大改变。对于高速流,计算技术的发展在某些方面领先于实验界验证结果的能力。由于这些技术适用于热化学非平衡流,因此应考虑本构关系的保真度。

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