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Journal ArticleDOI

Large-Eddy Simulations of a normal shock train in a constant-area isolator

Brandon Morgan, +2 more
- 18 Feb 2014 - 
- Vol. 52, Iss: 3, pp 539-558
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TLDR
In this article, a large-eddy simulation of a normal shock train in a constant-area isolator model (M∞=161, Reθ≈1660) is carried out to investigate solution sensitivity with respect to a variety of physical modeling assumptions.
Abstract
Large-eddy simulation of a normal shock train in a constant-area isolator model (M∞=161, Reθ≈1660) is carried out to investigate solution sensitivity with respect to a variety of physical modeling assumptions Simulations with spanwise periodic boundary conditions are first performed, the results of which are compared with experiment and validated with a three-level grid refinement study Due to the computational cost associated with resolving near-wall structures, the large-eddy simulation is run at a Reynolds number lower than that in the comparison experiment; thus, the confinement effect of the turbulent boundary layers is not exactly duplicated Although this discrepancy is found to affect the location of the first normal shock, the overall structure of the shock train and its interaction with the boundary layers matches the experiment quite closely Observations of pertinent physical phenomena in the experiment, such as a lack of reversed flow in the mean and the development of secondary shear laye

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Citations
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Inflow Turbulence Generation Methods

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Unstart phenomena induced by flow choking in scramjet inlet-isolators

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Three dimensional CFD investigation of shock train structure in a supersonic nozzle

TL;DR: In this paper, the authors investigated the shock train structure in a convergent-divergent nozzle using large eddy simulation (LES) methodology based on different subgrid models, including Smagorinsky-Lilly, wall-adapting local eddy-viscosity (WALE) and algebraic wall-model-based LES (WMLES).
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Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward Movement

TL;DR: In this paper, a numerical simulation was conducted using the commercial computational fluid dynamics software FLUENT to study the influence of inner flow structures on the motion characteristics of a separation oblique shock train caused by backpressure.
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Synthetic generation of equilibrium boundary layer turbulence from modeled statistics

TL;DR: An improved synthetic digital filtering method (SDFM) for the generation of equilibrium turbulence is described, with emphasis on the ease of application to complex configurations as mentioned in this paper, which facilitates the use of modeled (RANS) statistics for the mean flow and Reynolds stress profiles, instead of simulated (DNS or LES) statistics that are not readily available for three-dimensional flows.
References
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Compact finite difference schemes with spectral-like resolution

TL;DR: In this article, the authors present finite-difference schemes for the evaluation of first-order, second-order and higher-order derivatives yield improved representation of a range of scales and may be used on nonuniform meshes.
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A simple model for low-frequency unsteadiness in shock-induced separation

TL;DR: In this paper, a model to explain the low-frequency unsteadiness found in shock-induced separation is proposed for cases in which the flow is reattaching downstream, based on the properties of fluid entrainment in the mixing layer generated downstream of the separation shock whose lowfrequency motions are related to successive contractions and dilatations of the separated bubble.
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