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Juncture Flow Computations using kL-Based Turbulence ModelsThe development and implementation of kL-based Reynolds-Average Navier-Stokes (RANS) two-equation turbulence models are reported in this paper. The kL model is based on Abdol-Hamid's closure and Menter's modification to Rotta's two-equation model. Rotta showed that a reliable transport equation can be formed from the turbulence length scale L, and the turbulence kinetic energy k. Rotta's kL equation is well suited for a term-by-term modeling and displays useful features compared to other scale formulations. One of the important differences is the inclusion of higher-order velocity derivatives in the source terms of the scale equation. This can enhance the ability of RANS solvers to simulate unsteady flows in URANS mode. The k-kL scheme has been modified to include the Algebraic Reynolds Stress Model (ARSM) and the Quadratic Constitutive Relation (QCR) as nonlinear models. These models have gone through extensive validations using two-dimensional benchmark problems. The present study documents the application of the k-kL schemes to simulate flow around the Juncture Flow Model (JFM). The k-kL prediction results show generally good comparisons with measurements. The results from this formulation are similar to, or better than results using the SA-RC-QCR2000 two-equation turbulence model. The ARSM and the QCR formulations of k-kL show promise with a similar level of computational resources as basic two-equation turbulence models.
Document ID
20200002765
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
K S Abdol-Hamid ORCID
(Langley Research Center Hampton, Virginia, United States)
Nash’at N Ahmad
(Langley Research Center Hampton, Virginia, United States)
Jan-Renee Carlson
(Langley Research Center Hampton, Virginia, United States)
Robert T Biedron
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 20, 2020
Publication Date
January 6, 2020
Publication Information
Publication: AIAA SciTech 2020 Forum
Publisher: American Institute of Aeronautics and Astronautics
e-ISBN: 9781624105951
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-33124
AIAA 2020-1305
Meeting Information
Meeting: AIAA SciTech Exhibition and Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2020
End Date: January 10, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.07.01.05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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