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Turbulence Model Study for the Flow Around the NASA Common Research Model

Togiti, Vamshi and Eisfeld, Bernhard and Brodersen, Olaf (2014) Turbulence Model Study for the Flow Around the NASA Common Research Model. Journal of Aircraft, 51 (4), pp. 1331-1343. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C032609. ISSN 0021-8669.

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/full/10.2514/1.C032609


A turbulence model study was performed for the wing–body configuration of NASA’s common research model on common hybrid grids provided by the Fifth Drag Prediction Workshop Committee and on an in-house-generated hybrid grid. Here, eddy-viscosity models with and without quadratic constitution relation extension, which accounts for the anisotropy of normal turbulent stresses, and a differential Reynolds stress model were applied. In this paper, first, the influence of turbulence models on the prediction of side-of-body separation in the wing–body region and on the overall aerodynamic force and moment coefficients is discussed, and later, the influence of grid refinement on the predictions is presented. Finally, the effect of the quadratic constitution relation extension on the predictions of eddy-viscosity models is demonstrated and performance of different turbulence models is discussed by comparing numerical predictions with the experimental data from NASA’s National Transonic Facility.

Item URL in elib:https://elib.dlr.de/90391/
Document Type:Article
Additional Information:July-August 2014, Published online: 29 May 2014
Title:Turbulence Model Study for the Flow Around the NASA Common Research Model
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Date:July 2014
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
Page Range:pp. 1331-1343
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
Keywords:CRM, Turbulence model study, Reynolds stress model, eddy viscosity models, QCR
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Togiti, Vamshi
Deposited On:03 Sep 2014 13:21
Last Modified:29 Nov 2023 13:18

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