2018 AIAA Aerospace Sciences Meeting 2018
DOI: 10.2514/6.2018-2092
|View full text |Cite
|
Sign up to set email alerts
|

An Algebraic Wall-Model for Large Eddy Simulation With the FR/CPR Method

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

0
6
1

Year Published

2024
2024
2024
2024

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(7 citation statements)
references
References 26 publications
0
6
1
Order By: Relevance
“…There was no significant difference between other auxiliary conditions. Unlike in the previous study, 19 no deviation was observed with the "No-slip" condition. To better clarify the effect of the auxiliary wall boundary conditions, the mean velocity and velocity gradients below the matching points (y∕𝛿 ≲ 0.1) are compared in Figure 9.…”
Section: Equilibrium Turbulent Channel Flow (Re 𝝉 ≈ 5200)contrasting
confidence: 90%
See 4 more Smart Citations
“…There was no significant difference between other auxiliary conditions. Unlike in the previous study, 19 no deviation was observed with the "No-slip" condition. To better clarify the effect of the auxiliary wall boundary conditions, the mean velocity and velocity gradients below the matching points (y∕𝛿 ≲ 0.1) are compared in Figure 9.…”
Section: Equilibrium Turbulent Channel Flow (Re 𝝉 ≈ 5200)contrasting
confidence: 90%
“…Previous studies have reported deteriorated prediction accuracy and stability due to higher-order polynomial approximations. 14,18,19 Since the WMLES grid does not resolve large velocity gradients in the inner layer, using high-order polynomial approximations for velocity profiles often causes large oscillations, 14 leading to errors and instability. In high-order finite difference methods, the velocity gradient is usually evaluated by a low-order one-sided difference scheme.…”
Section: Introductionmentioning
confidence: 99%
See 3 more Smart Citations