To read this content please select one of the options below:

Parametric and V&V study in a fundamental CFD process: revisiting the lid-driven cavity flow

Mingming Ge (Kevin T. Crofton Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia, USA)
Xin-Lei Zhang (The State Key Laboratory of Nonlinear Mechanics, Institute of Mechanics, Chinese Academy of Sciences, Beijing, China)
Kaleb Brookshire (Kevin T. Crofton Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia, USA)
Olivier Coutier-Delgosha (Kevin T. Crofton Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia, USA)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 24 December 2021

Issue publication date: 23 March 2022

162

Abstract

Purpose

The openings on aircraft structures can be modeled from an aerodynamical point of view as lid-driven cavities (LDC). This paper aims to show the primary verification and validation (V&V) process in computational fluid dynamics (CFD, and to investigate the influences of numerical settings on the efficiency and accuracy for solving the LDC problem.

Design/methodology/approach

To dig into the details of CFD approaches, this paper outlines the design, implementation, V&V and results of an efficient explicit algorithm. The parametric study is performed thoroughly focusing on various iteration methods, grid density discretization terms and Reynolds number effects.

Findings

This study parameterized the numerical implementation which provides empirical insights into how computational accuracy and efficiency are affected by changing numerical settings. At a low Reynolds number (not over 1,000), the time-derivative preconditioning is necessary, and k = 0.1 can be the optimal value to guarantee the efficiency, as well as the stability. A larger artificial viscosity (c = 1/16) would relieve the calculating oscillation issue but proportionally increase the discretization error. Furthermore, the iteration method and the mesh quality are two key factors that affect the convergence efficiency, thus need to be selected “wisely”.

Practical implications

The study shows how numerical implementation can enhance an accurate and efficient solution. This workflow can be used to determine the best parameter settings whenever CFD researchers applying this LDC problem as a complementary design tool for testing newly developed solvers.

Originality/value

The studied LDC problem is representative of CFD analysis in real aircraft structures. These numerical simulations provide a cost-effective and convenient tool to understand the parameter sensitivity, solution receptivity and physics of the CFD process.

Keywords

Acknowledgements

This work was supported by the Office of Naval Research [grant number N00014-18-S-B001]. The authors would like to thank Dr. Ki-Han Kim from the Office of Naval Research for the continuous support.

Citation

Ge, M., Zhang, X.-L., Brookshire, K. and Coutier-Delgosha, O. (2022), "Parametric and V&V study in a fundamental CFD process: revisiting the lid-driven cavity flow", Aircraft Engineering and Aerospace Technology, Vol. 94 No. 4, pp. 515-530. https://doi.org/10.1108/AEAT-04-2021-0108

Publisher

:

Emerald Publishing Limited

Copyright © 2021, Emerald Publishing Limited

Related articles