Grid Influence on Turbulence Model Coefficient Uncertainties in Transonic Wall-Bounded Flows
Abstract
The goal of this work is to determine the effect of grid topology and flow solver discretization on the uncertainty quantification and sensitivity analysis of commonly used turbulence models in Reynolds-averaged Navier-Stokes codes due to uncertainty in the values of turbulence model coefficients as well as to rank the contribution of each coefficient to uncertainty in various output quantities of interest for transonic flow over an RAE 2822 airfoil. Three turbulence models were considered: Spalart-Allmaras, 2006 Wilcox k-ω, and Menter shear-stress transport. Several structured and unstructured grid topologies were employed in the analysis. The FUN3D code of NASA Langley Research Center and the BCFD code of the Boeing Company were used as the flow solvers. The uncertainty analysis employed stochastic expansions based on nonintrusive polynomial chaos for efficient uncertainty propagation. Sobol indices were used to rank the relative contributions of each coefficient to the total uncertainty in the output quantities of interest. The solutions obtained with all grids and computational-fluid-dynamics codes identified a common set of coefficients for each turbulence model that influence the output uncertainty significantly for transonic wall-bounded flows.
Recommended Citation
J. Schaefer et al., "Grid Influence on Turbulence Model Coefficient Uncertainties in Transonic Wall-Bounded Flows," AIAA Journal, vol. 56, no. 8, pp. 3123 - 3137, American Institute of Aeronautics and Astronautics (AIAA), May 2018.
The definitive version is available at https://doi.org/10.2514/1.J056225
Department(s)
Mechanical and Aerospace Engineering
Research Center/Lab(s)
Center for High Performance Computing Research
Keywords and Phrases
Codes (symbols); Computational fluid dynamics; Flow simulation; Navier Stokes equations; Reynolds equation; Sensitivity analysis; Shear stress; Stochastic systems; Supersonic aircraft; Turbulence models; Wall flow, Computational Fluid Dynamics codes; Quantities of interests; Relative contribution; Reynolds averaged navier stokes codes; Shear-stress transport; Turbulence model coefficients; Uncertainty propagation; Uncertainty quantifications, Uncertainty analysis
International Standard Serial Number (ISSN)
0001-1452; 1533-385X
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2018 The Boeing Company, All rights reserved.
Publication Date
01 May 2018
Comments
The partial support for the first author and the support for last author for this research are provided under NASA grant NNX14AN17A (Mujeeb Malik, program monitor).