A Wall Function for Turbulent Boundary Layers under Rotation via Symbolic Regression
Pith reviewed 2026-06-27 21:16 UTC · model grok-4.3
The pith
Symbolic regression derives compact wall-function expressions that capture how Coriolis forces deflect turbulent boundary layers differently on leading and trailing sides under system rotation.
A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.
Core claim
The central claim is that symbolic regression, trained on the deflection behavior of turbulent boundary layers, yields physically interpretable wall-function expressions valid over a wide range of rotation numbers; these expressions show that increasing rotation contracts the leading-side boundary layer, expands the trailing-side layer, and drives the leading side toward relaminarization, matching high-fidelity numerical results.
What carries the argument
Symbolic regression applied to the deflection behavior of turbulent boundary layers to generate rotation-dependent analytical wall functions.
If this is right
- The wall functions are compact and remain interpretable across rotation numbers.
- They reproduce the contraction of the leading-side boundary layer and expansion on the trailing side.
- The leading side shows a tendency toward relaminarization as rotation intensifies.
- The expressions complement conventional wall functions and supply a new route for turbulence-model closure under system rotation.
Where Pith is reading between the lines
- The same regression procedure could be applied to other body-force effects such as buoyancy or curvature to produce analogous closed-form corrections.
- Integration of these explicit functions into RANS codes would allow rotation effects to be included without additional sub-grid modeling.
- The approach supplies a route to test whether other non-equilibrium wall laws can be recovered in closed form from limited simulation data.
Load-bearing premise
The symbolic regression produces expressions that remain valid and physically interpretable over a wide range of rotation numbers.
What would settle it
Comparison of the derived wall functions against independent DNS or LES data at rotation numbers outside the range used to generate the expressions would confirm or refute their accuracy.
Figures
read the original abstract
This study employs symbolic regression to derive physically interpretable, white-box wall-function expressions for turbulent boundary layers under system rotation. Flows in a rotating frame are subject to Coriolis forces, which deflect the boundary layer profile from static case. The classical law of the wall, formulated under non-rotating conditions, is ill-suited to describing the effects of rotation. To obtain the wall function under rotation, we examine the deflection behavior of the turbulent boundary layers on the leading and trailing sides, and construct wall functions that are valid over a wide range of rotation numbers. The analytical expressions show that, as the rotation effect intensifies, the boundary layer on the leading side contracts whereas that on the trailing side expands, and the leading side exhibits a tendency towards relaminarization, consistent with high-fidelity numerical results. The resulting symbolic expressions are compact and interpretable. The wall functions obtained in this study complement conventional wall functions, and provide a new avenue for turbulence model closure subject to system rotation.
Editorial analysis
A structured set of objections, weighed in public.
Referee Report
Summary. This paper employs symbolic regression to derive physically interpretable wall-function expressions for turbulent boundary layers under system rotation. By examining deflection behavior on leading and trailing sides from simulation data, it constructs expressions claimed to be valid over a wide range of rotation numbers. These show boundary-layer contraction on the leading side, expansion on the trailing side, and a relaminarization tendency on the leading side, stated to be consistent with high-fidelity numerical results. The expressions are presented as compact, white-box complements to conventional wall functions for turbulence closure under rotation.
Significance. If the expressions prove generalizable, the work supplies an interpretable, data-derived alternative for incorporating Coriolis effects into near-wall modeling, which could aid RANS closures in rotating machinery flows. The emphasis on physical interpretability distinguishes it from purely black-box approaches. However, because the derivation is entirely data-driven, significance depends on demonstrated generalization beyond training data, which is not established in the manuscript.
major comments (2)
- [Method (symbolic regression procedure)] The manuscript provides no details on the symbolic regression algorithm employed, the criteria for selecting training data (e.g., specific rotation numbers or deflection metrics), or quantitative validation metrics such as hold-out error or cross-validation scores. This information is load-bearing for the central claim that the expressions remain valid over a wide range of rotation numbers and reproduce high-fidelity behavior.
- [Results and validation] No independent hold-out tests, cross-validation across rotation numbers, or extrapolation checks for rotation numbers outside the training range are reported. Without these, the consistency statements with high-fidelity results and the relaminarization tendency risk being circular, as the fitted expressions may simply reproduce the input data rather than predict new behavior.
minor comments (2)
- [Abstract] The abstract refers to 'high-fidelity numerical results' without citing the specific simulations, parameters, or references used for comparison.
- [Results] Notation for the derived wall functions (e.g., any new symbols for rotation-modified velocity or length scales) should be introduced with explicit definitions and units in the first results section.
Simulated Author's Rebuttal
We thank the referee for the constructive comments highlighting the need for greater methodological transparency and validation. We agree these elements are essential to substantiate the claims of generalizability and will incorporate the requested details and tests in the revised manuscript.
read point-by-point responses
-
Referee: [Method (symbolic regression procedure)] The manuscript provides no details on the symbolic regression algorithm employed, the criteria for selecting training data (e.g., specific rotation numbers or deflection metrics), or quantitative validation metrics such as hold-out error or cross-validation scores. This information is load-bearing for the central claim that the expressions remain valid over a wide range of rotation numbers and reproduce high-fidelity behavior.
Authors: We agree that the original manuscript omitted key details on the symbolic regression procedure. In the revision we will add a dedicated methods subsection specifying the algorithm (including any software implementation), the exact criteria used to select training data (rotation numbers, deflection metrics, and data sources), and quantitative metrics such as hold-out error and cross-validation scores. These additions will directly support the claim of validity across a wide range of rotation numbers. revision: yes
-
Referee: [Results and validation] No independent hold-out tests, cross-validation across rotation numbers, or extrapolation checks for rotation numbers outside the training range are reported. Without these, the consistency statements with high-fidelity results and the relaminarization tendency risk being circular, as the fitted expressions may simply reproduce the input data rather than predict new behavior.
Authors: We acknowledge the validity of this concern. The revised manuscript will include independent hold-out tests, cross-validation performed across distinct rotation numbers, and extrapolation checks for rotation numbers beyond the training range. These results will be presented to demonstrate that the derived expressions capture the observed physical trends (boundary-layer contraction/expansion and relaminarization) rather than merely reproducing the training data. revision: yes
Circularity Check
Symbolic regression wall functions fitted to high-fidelity data reproduce its behaviors by construction
specific steps
-
fitted input called prediction
[Abstract]
"The analytical expressions show that, as the rotation effect intensifies, the boundary layer on the leading side contracts whereas that on the trailing side expands, and the leading side exhibits a tendency towards relaminarization, consistent with high-fidelity numerical results."
Expressions are obtained by symbolic regression trained on the examined deflection behavior of the same turbulent boundary layer data. Their reproduction of contraction/expansion and relaminarization is therefore a direct encoding of the training patterns, not an independent prediction or derivation.
full rationale
The paper derives wall-function expressions exclusively via symbolic regression on deflection data from high-fidelity simulations of rotating boundary layers. Its central claim—that the resulting expressions demonstrate leading-side contraction, trailing-side expansion, and relaminarization tendency, and remain valid over wide rotation numbers—is presented as an analytical finding. Because the regression directly encodes the input data patterns, this consistency is tautological rather than independently derived. No hold-out validation, extrapolation tests, or external first-principles justification is described that would break the reduction to the training inputs.
Axiom & Free-Parameter Ledger
Reference graph
Works this paper leans on
-
[1]
J. H. Wagner, B. V. Johnson, T. J. Hajek. Heat Transfer in Rotating Passages With Smooth Walls and Radial Outward Flow. Journal of Turbomachinery, vol. 113, pp. 42 -51, 1991
1991
-
[2]
K. Wei, Z. Tao, H. W. Deng, R. Q. You, editors. Interaction of secondary flow with developing, turbulent boundary layers in a rotating duct. Proceedings of The American Society of Mechanical Engineers Turbomachinery Technical Conference & Exposition 2015; 2015; Montreal, Quebec. Montreal, Quebec, CanadaASME Turbo Expo 2015: Turbine Technical Conference an...
2015
-
[3]
K. Wei, Z. Tao, R. You, H. Wu, H. Li. Development of a turbulent boundary layer in a rotating square cross -section channel with relatively high local rotation parameter. Exp Therm Fluid Sci, vol. 86, pp. 85 -97, 2017
2017
-
[4]
G. F. Li, Z. Tao, H. J. Wu, R. Q. You, H. W. Li, editors. Experimental investigation on boundary layer flow under the effect of temperature gradient in a smooth rotating channel using hot -wire. Proceedings of The American Society of Mechanical Engineers Tu rbomachinery Technical Conference & Exposition 2018; 2018; Pittsburgh, Pennsylvania. Volume 8B: Hea...
2018
-
[5]
Z. Tao, H. Wu, R. You, H. Li, K. Wei. Turbulent characteristics and rotation correction of wall function in rotating channel with high local rotation parameter. Chin J Aeronaut, vol. 31, pp. 1985 -99, 2018
1985
-
[6]
R. Q. You, K. Wei, Z. Tao, H. W. Li, G. Q. Xu. Development of secondary flow field under rotating condition in a straight channel with square cross-section. Chin J Aeronaut, vol. 31, pp. 1703 -15, 2018
2018
-
[7]
Z. Y. Jiang, H. W. Li, R. Q. You. Experiment on turbulent flow in rotating smooth channel with 1D hot wire. J Aerosp Power, vol. 34, pp. 556 -66, 2019
2019
-
[8]
H. Li, Z. Jiang, Z. Tao, R. You, H. Wu. Effect of system rotating on turbulent boundary layer flow. Int J Heat Fluid Flow, vol. 75, pp. 185 -94, 2019
2019
-
[9]
J. H. G. Howard, S. V. Patankar, R. M. Bordynuik. Flow Prediction in Rotating Ducts Using Coriolis -Modified Turbulence Models. ASME J Fluids Eng, vol. 102, pp. 456-61, 1980
1980
-
[10]
A. K. Majumdar, V. S. Pratap, D. B. Spalding. Numerical Computation of Flow in Rotating Ducts. In: Patankar SV, Pollard A, Singhal AK, Vanka SP, editors. Numerical Prediction of Flow, Heat Transfer, Turbulence and Combustion: Pergamon; 1983. p. 211 -6
1983
-
[11]
B. E. Launder, D. P. Tselepidakis, B. A. Younis. A second -moment closure study of rotating channel flow. J Fluid Mech, vol. 183, pp. 63 -75, 1987
1987
-
[12]
C. G. Speziale. Turbulence Modeling in Noninertial Frames of Reference. Theoretical and Computational Fluid Dynamics, vol. 1, pp. 3 -19, 1989
1989
-
[13]
Prakash, R
C. Prakash, R. Zerkle. Prediction of Turbulent Flow and Heat Transfer in a Radially Rotating Square Duct. Journal of Turbomachinery, vol. 114, pp. 835-46, 1992
1992
-
[14]
H. Z. Asan. A computational study of laminar and turbulent flows in rotating rectangular ducts [Dissertation/Thesis]1993
1993
-
[15]
Tekriwal
P. Tekriwal. Heat Transfer Predictions With Extended k –ε Turbulence Model in Radial Cooling Ducts Rotating in Orthogonal Mode. Journal of Heat Transfer, vol. 116, pp. 369 -80, 1994
1994
-
[16]
Tekriwal
P. Tekriwal. Heat Transfer Predictions in Rotating Radial Smooth Channel: Comparative Study of k-ε Models With Wall Function and Low- Re Model. Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration1994
-
[17]
Bredberg, editor Turbulence Modelling for Internal Cooling of Gas - Turbine Blades2002
J. Bredberg, editor Turbulence Modelling for Internal Cooling of Gas - Turbine Blades2002
-
[18]
Jakirlic, K
S. Jakirlic, K. Hanjalic, C. Tropea. Modeling Rotating and Swirling Turbulent Flows: A Perpetual Challenge. AIAA J, vol. 40, pp. 1984 -96, 2002
1984
-
[19]
H. Liao, X. Sun, Y. Liu, W. Zhang. Data -driven turbulence modeling: A mutually coupled framework for symbolic regression and data assimilation. Phys Fluids, vol. 37, pp. 075211, 2025
2025
-
[20]
Z. Yang, X. Shan, X. I. A. Yang, W. Zhang. Data -enabled discovery of specific and generalisable turbulence closures. J Fluid Mech, vol. 1016, pp. R1, 2025
2025
-
[21]
H. Wu, R. Chen, Y. Ye, J. Lou, Z. Yin, S. Zhou, et al. Modeling of wall function based on symbolic regression under streamwise pressure gradient. Aerospace Science and Technology, vol. 168, pp. 111107, 2026
2026
-
[22]
J. Kim, P. Moin, R. Moser. Turbulence statistics in fully developed channel flow at low Reynolds number. J Fluid Mech, vol. 177, pp. 133 - 66, 1987
1987
-
[23]
Z. Tao, R. You, Y. Ma, H. Li. Temperature and velocity characteristics of rotating turbulent boundary layers under non-isothermal conditions. Phys Fluids, vol. 34, pp. 065138, 2022
2022
discussion (0)
Sign in with ORCID, Apple, or X to comment. Anyone can read and Pith papers without signing in.