Closed form solution of plane turbulent boundary flow – solution process, validity conditions and extension

Abstract The Prandtl mixing length plane turbulent boundary flow is governed by the nonlinear ordinary differential equation (ODE): <m:math xmlns:m="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <m:mfrac> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>u</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>y</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> </m:mfrac> <m:mo>+</m:mo> <m:msup> <m:mrow> <m:mi>κ</m:mi> </m:mrow> <m:mrow> <m:mn>2</m:mn> </m:mrow> </m:msup> <m:msup> <m:mrow> <m:msup> <m:mrow> <m:mi>y</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> <m:mrow> <m:mn>2</m:mn> </m:mrow> </m:msup> <m:msup> <m:mrow> <m:mfenced close=")" open="("> <m:mrow> <m:mfrac> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>u</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>y</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> </m:mfrac> </m:mrow> </m:mfenced> </m:mrow> <m:mrow> <m:mn>2</m:mn> </m:mrow> </m:msup> <m:mo>=</m:mo> <m:mn>1</m:mn> </m:math> $\frac{\mathrm{d}{u}^{+}}{\mathrm{d}{y}^{+}}+{\kappa }^{2}{{y}^{+}}^{2}{\left(\frac{\mathrm{d}{u}^{+}}{\mathrm{d}{y}^{+}}\right)}^{2}=1$ with boundary condition y + = 0 : u + = 0. Although van Driest first derived the closed-form solution for this ODE in 1956 (E. R. van Driest, “On turbulent flow near a wall,” J. Aeronaut. Sci. , vol. 23, no. 11, pp. 1007–1011, 1956), but the lack of detailed solution process led to its long-term neglect in subsequent fluid mechanics textbooks and research. As a result, the problem of finding the solution has remained an open question in the community. In this work, we independently rederive the solution and provide a complete, step-by-step solution process. Furthermore, we explicitly clarify the validity conditions of the solution (i.e., smooth wall, zero pressure gradient, fully developed turbulent flow, incompressible flow) and propose a modified analytical extension that conforms well to direct numerical simulation (DNS) results. The proposed modification incorporating van Driest-type damping into the solution framework is physically motivated, and this extension is semi-empirical, thus should be interpreted as a model enhancement/refinement rather than an exact mathematical solution. The present work not only supplements the missing solution details of van Driest’s solution but also improves its applicability.

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Publication Details

Journal
Transport Phenomena
Published
2026-02-03
DOI
https://doi.org/10.1515/tp-2026-0014
Primary Topic
Computational Fluid Dynamics and Aerodynamics
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article
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article

Closed form solution of plane turbulent boundary flow – solution process, validity conditions and extension

Bo Hua Sun
Transport Phenomena
Computational Fluid Dynamics and Aerodynamics
article

Closed form solution of plane turbulent boundary flow – solution process, validity conditions and extension

Bo Hua Sun
article en

Abstract

Abstract The Prandtl mixing length plane turbulent boundary flow is governed by the nonlinear ordinary differential equation (ODE): <m:math xmlns:m="http://www.w3.org/1998/Math/MathML" overflow="scroll"> <m:mfrac> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>u</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>y</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> </m:mfrac> <m:mo>+</m:mo> <m:msup> <m:mrow> <m:mi>κ</m:mi> </m:mrow> <m:mrow> <m:mn>2</m:mn> </m:mrow> </m:msup> <m:msup> <m:mrow> <m:msup> <m:mrow> <m:mi>y</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> <m:mrow> <m:mn>2</m:mn> </m:mrow> </m:msup> <m:msup> <m:mrow> <m:mfenced close=")" open="("> <m:mrow> <m:mfrac> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>u</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> <m:mrow> <m:mi mathvariant="normal">d</m:mi> <m:msup> <m:mrow> <m:mi>y</m:mi> </m:mrow> <m:mrow> <m:mo>+</m:mo> </m:mrow> </m:msup> </m:mrow> </m:mfrac> </m:mrow> </m:mfenced> </m:mrow> <m:mrow> <m:mn>2</m:mn> </m:mrow> </m:msup> <m:mo>=</m:mo> <m:mn>1</m:mn> </m:math> $\frac{\mathrm{d}{u}^{+}}{\mathrm{d}{y}^{+}}+{\kappa }^{2}{{y}^{+}}^{2}{\left(\frac{\mathrm{d}{u}^{+}}{\mathrm{d}{y}^{+}}\right)}^{2}=1$ with boundary condition y + = 0 : u + = 0. Although van Driest first derived the closed-form solution for this ODE in 1956 (E. R. van Driest, “On turbulent flow near a wall,” J. Aeronaut. Sci. , vol. 23, no. 11, pp. 1007–1011, 1956), but the lack of detailed solution process led to its long-term neglect in subsequent fluid mechanics textbooks and research. As a result, the problem of finding the solution has remained an open question in the community. In this work, we independently rederive the solution and provide a complete, step-by-step solution process. Furthermore, we explicitly clarify the validity conditions of the solution (i.e., smooth wall, zero pressure gradient, fully developed turbulent flow, incompressible flow) and propose a modified analytical extension that conforms well to direct numerical simulation (DNS) results. The proposed modification incorporating van Driest-type damping into the solution framework is physically motivated, and this extension is semi-empirical, thus should be interpreted as a model enhancement/refinement rather than an exact mathematical solution. The present work not only supplements the missing solution details of van Driest’s solution but also improves its applicability.

Transport Phenomena
Beijing Institute of Nanoenergy and Nanosystems (CN), University of Chinese Academy of Sciences (CN)
Openalex Percentile: Top 66%
Computational Fluid Dynamics and Aerodynamics
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