Hybrid LES/RANS Simulation of a 10-degree Double-fin Crossing Shock Flow at Mach 8.28 PDF Download
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Author: John Arthur Boles
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Keywords: hybrid turbulence model, high-speed flow, flow modeling, shockwave boundary layer interaction, turbulent boundary layer, CFD, LES, turbulence, turbulence modeling.
Author: John Arthur Boles
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
Keywords: hybrid turbulence model, high-speed flow, flow modeling, shockwave boundary layer interaction, turbulent boundary layer, CFD, LES, turbulence, turbulence modeling.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
The simulation of a Mach 8.28 10-degree double-fin crossing shock flow using a hybrid large-eddy ⁄ Reynolds-averaged Navier-Stokes (LES⁄RANS) solver is presented in this work. The solver blends a Menter two-equation model for RANS with a Yoshizawa one-equation subgrid model for the LES calculations. The solver uses a flow-dependent transition function based on wall distance and a modeled form of the Taylor microscale. Turbulent boundary layers are initiated and sustained in the inflow region using a recycling⁄rescaling technique applied to the fluctuation fields. The hybrid LES⁄RANS model is tested using both Menter's Baseline (BSL) and Shear Stress Transport (SST) models for the RANS closure. These results are compared to pure Menter BSL and SST RANS results as well as with the experimental data of Kussoy and Horstman(1992). This study concludes that while the hybrid LES⁄RANS model outperforms RANS calculations in the inflow region where the flow is nominally two-dimensional, it significantly overpredicts the wall heat transfer rates in the region of the crossing shock interaction. Possible explanations for this behavior as well as plans for future attempts at solutions to these shortcomings are provided.
Author: Thomas C. Fan
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Rajib Roy
Publisher:
ISBN: 9780355318883
Category : Turbulent boundary layer
Languages : en
Pages : 119
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Book Description
Numerical modeling of turbulent flows needs to be accurate yet fast and cost effective for practical applications. For flows with boundary layer separation the Large Eddy Simulation (LES) method provides accurate results but the computational cost increases fast with the Reynolds number due to the near wall resolution requirement. To alleviate the cost burden, a statistical (RANS) method can be incorporated in a LES method to build a hybrid model, which applies RANS in the near wall attached flow region (to reduce cost) and LES in the separated flow region (to increase accuracy). In this work, a novel second-moment closure based hybrid RANS-LES model is used to improve the overall accuracy. The new hybrid model coefficients are calibrated in a canonical attached flow and the model is then applied in several other attached and separated turbulent flow cases to evaluate the model performance.Y
Author: Bharanidharan Rajamani
Publisher:
ISBN:
Category :
Languages : en
Pages : 332
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Author: Mohammad Faridul Alam
Publisher:
ISBN:
Category : Science
Languages : en
Pages :
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The objective of this study is to evaluate a recently proposed dynamic hybrid Reynolds-averaged Navier-Stokes (RANS)-Large Eddy Simulation (LES) modeling framework that seeks to effectively address issues regarding RANS-to-LES transition and explicit grid dependence inherent in most current hybrid RANS-LES (HRL) models. RANS-to-LES transition in the investigated dynamic HRL (DHRL) model is based on the physical concept of maintaining continuity of total turbulence production using two rigorously separated turbulent stress parameters, where one is obtained from the RANS model and the other from the LES model. Computations of two canonical test cases-two-dimensional turbulent channel flow and backward facing step flow-were performed to assess the potential of the DHRL model for predicting both attached and separated turbulent flows. This investigation attempts to evaluate the ability of the DHRL method to reproduce the detailed physics of attached and separated turbulent flows, as well as to resolve the issues concerning log-layer mismatch and delayed break down of separated shear layers. The DHRL model simulation results are compared with experimental and DNS data, along with the computational results for other HRL and RANS models. In summary, these comparisons demonstrate that the DHRL framework does address many of the weaknesses inherent in most current HRL models.
Author: Mohammad Faridul Alam
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
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Book Description
A dynamic hybrid Reynolds-averaged Navier-Stokes (RANS)-Large Eddy Simulation (LES) modeling framework has been investigated and further developed to improve the Computational Fluid Dynamics (CFD) prediction of turbulent flow features along with laminar-to-turbulent transitional phenomena. In recent years, the use of hybrid RANS/LES (HRL) models has become more common in CFD simulations, since HRL models offer more accuracy than RANS in regions of flow separation at a reduced cost relative to LES in attached boundary layers. The first part of this research includes evaluation and validation of a dynamic HRL (DHRL) model that aims to address issues regarding the RANS-to-LES zonal transition and explicit grid dependence, both of which are inherent to most current HRL models. Simulations of two test cases—flow over a backward facing step and flow over a wing with leading-edge ice accretion—were performed to assess the potential of the DHRL model for predicting turbulent features involved in mainly unsteady separated flow. The DHRL simulation results are compared with experimental data, along with the computational results for other HRL and RANS models. In summary, these comparisons demonstrate that the DHRL framework does address many of the weaknesses inherent in most current HRL models. Although HRL models are widely used in turbulent flow simulations, they have limitations for transitional flow predictions. Most HRL models include a fully turbulent RANS component for attached boundary layer regions. The small number of HRL models that do include transition-sensitive RANS models have issues related to the RANS model itself and to the zonal transition between RANS and LES. In order to address those issues, a new transition-sensitive HRL modeling methodology has been developed that includes the DHRL methodology and a physics-based transition-sensitive RANS model. The feasibility of the transition-sensitive dynamic HRL (TDHRL) model has been investigated by performing numerical simulations of the flows over a circular cylinder and a PAK-B airfoil. Comparisons with experimental data along with computational results from other HRL and RANS models illustrate the potential of TDHRL model for accurately capturing the physics of complex transitional flow phenomena.
Author: David C. Wilcox
Publisher:
ISBN: 9781928729082
Category : Fluid dynamics
Languages : en
Pages : 522
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Author: Holger Babinsky
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
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Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Author: Jesse Ambrose Fulton
Publisher:
ISBN:
Category :
Languages : en
Pages : 173
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