Work

Contributions to the Sixth Drag Prediction Workshop Using Structured, Overset Grid Methods

Year: 2017

Type: article

Abstract: Structured-grid solutions obtained for the NASA Common Research Model for the Sixth AIAA Computational Fluid Dynamics Drag Prediction Workshop are detailed. Three different flow solvers were used among the contributors, and the numerical methodologies and turbulence modeling strategies employed by each code are described. Key results for all authors include grid convergence studies for the drag increment of a nacelle and pylon added to a wing–body configuration and a buffet study accounting for static aeroelastic deformation. Additional studies performed include feature-based adaptive mesh refinement and higher-order convective flux discretization, among others.

Source: Journal of Aircraft

DOI: 10.2514/1.c034486

Authors: James G. Coder, David Hue, Gaetan Kenway, Thomas H. Pulliam, Anthony J. Sclafani, Leonel Serrano, John C. Vassberg

Institutions: University of Tennessee at Knoxville, Ames Research Center, Office National d'Études et de Recherches Aérospatiales, Boeing (United States), University of Michigan

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: green

Funders: Boeing, National Aeronautics and Space Administration, University of Michigan, Pennsylvania State University, Office National d'études et de Recherches Aérospatiales

OpenAlex ID: W2766710120

FWCI: 0.416

Cites: 29

Cited by: 7

Related to: 10