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Nonlinear evolution of vortical disturbances entrained in the entrance region of a circular pipe – CORRIGENDUM

Published online by Cambridge University Press:  14 July 2025

Kaixin Zhu
Affiliation:
School of Mechanical, Aerospace and Civil Engineering, The University of Sheffield, Sheffield S1 3JD, UK
Pierre Ricco*
Affiliation:
School of Mechanical, Aerospace and Civil Engineering, The University of Sheffield, Sheffield S1 3JD, UK
*
Corresponding author: Pierre Ricco, p.ricco@sheffield.ac.uk

Abstract

Information

Type
Corrigendum
Copyright
© The Author(s), 2025. Published by Cambridge University Press

In our recent work Zhu & Ricco (Reference Zhu and Ricco2024), the nonlinear unsteady boundary-region equations (2.15)–(2.18), governing the formation and evolution of the perturbation flow in the entrance region of a circular pipe, are derived.

For the case of nonzero spanwise wavenumber $m\neq 0$ in § 2.3.1., the pressure $\hat {p}_{m,n}$ and the azimuthal velocity $\hat {w}_{m,n}$ are eliminated from the $r$ -momentum equation for convenience of the numerical calculations, resulting in equation (2.27) in Zhu & Ricco (2024). However, one nonlinear term in equation (2.27) is missing. The correct version of equation (2.27) is

(0.1) \begin{align} \widehat {V}\hat {v}_{m,n} & + \widehat {V}_r\frac {\partial \hat {v}_{m,n}}{\partial r} + \widehat {V}_x\frac {\partial \hat {v}_{m,n}}{\partial \bar {x}} + \widehat {V}_{rr}\frac {\partial ^2 \hat {v}_{m,n}}{\partial r^2} + \widehat {V}_{xr}\frac {\partial ^2 \hat {v}_{m,n}}{\partial \bar {x}\partial r} + \widehat {V}_{rrr}\frac {\partial ^3 \hat {v}_{m,n}}{\partial r^3} + \widehat {V}_{xrr}\frac {\partial ^3 \hat {v}_{m,n}}{\partial \bar {x}\partial r^2} \nonumber \\ & + \widehat {V}_{rrrr}\frac {\partial ^4 \hat {v}_{m,n}}{\partial r^4} + \hat {U}\hat {u}_{m,n} + \widehat {U}_r\frac {\partial \hat {u}_{m,n}}{\partial r} + \widehat {U}_x\frac {\partial \hat {u}_{m,n}}{\partial \bar {x}} + \widehat {U}_{rr}\frac {\partial ^2 \hat {u}_{m,n}}{\partial r^2} + \widehat {U}_{xr}\frac {\partial ^2 \hat {u}_{m,n}}{\partial \bar {x}\partial r} \nonumber\\ & + \widehat {U}_{xrr}\frac {\partial ^3 \hat {u}_{m,n}}{\partial \bar {x}\partial r^2} = \fbox{$r_t\dfrac {2r}{m^2}\dfrac {\partial \hat {\mathcal{X}}_{m,n}}{\partial \bar {x}}$} + r_t\frac {r^2}{m^2}\frac {\partial ^2 \hat {\mathcal{X}}_{m,n}}{\partial \bar {x}\partial r} + r_t\hat {\mathcal{Y}}_{m,n} + \frac {ir_t}{m}\frac {\partial \left (r\hat {\mathcal{Z}}_{m,n}\right )}{\partial r}, \\[-12pt] \nonumber \end{align}

where the missing term is boxed.

Numerical simulations were repeated with the missing term included and its contribution to the results was found to be very small. The discussion of the results and the conclusions in Zhu & Ricco (Reference Zhu and Ricco2024) are therefore unaffected. We have reproduced figures 36, 7(c) and 7(d) in Zhu & Ricco (Reference Zhu and Ricco2024) with our corrected solver. The following figures present a comparison between the original results (shown in blue) and the corrected results (shown in black and red). Figure 16 is also reproduced, with different values of $\epsilon$ chosen to achieve a better agreement with the experimental data.

Figure 3. Comparison between the original results (blue lines) and the corrected results (black lines). Only the nonlinear results are presented as the linear results are unaffected.

Figure 4. Comparison between the original results (blue lines) and the corrected results (black lines).

Figure 5. Comparison between the original results (blue lines) and the corrected results (black lines).

Figure 6. Comparison between the original results (blue lines) and the corrected results (black and red lines).

Figure 7. $(c)$ and $(d)$ Comparison between the original results (blue lines) and the corrected results (black lines).

Figure 16. Comparison of $(a)$ the mean flow and $(b)$ the perturbation flow between the experimental measurements (circles) and our numerical results (lines). Open and solid circles: experimental data measured by Wygnanski & Champagne (Reference Wygnanski and Champagne1973) (refer to as WC73 in the figure) with $(u_{rms}/\bar {U})_{cl}=5.8\,\%$ and $7.8\,\%$ . Dotted and solid lines: present results with the new values $\epsilon =0.05$ , $0.09$ . The other parameters are unvaried: $Re_R=1200$ , $x_R = 30$ , $k_{x\kern-1pt,\kern-1pt R}=0.118$ , $l=2$ and $m_0=2$ .

References

Wygnanski, I.J. & Champagne, F.H. 1973 On transition in a pipe. Part 1. The origin of puffs and slugs and the flow in a turbulent slug. J. Fluid Mech. 59 (2), 281335.10.1017/S0022112073001576CrossRefGoogle Scholar
Zhu, K. & Ricco, P. 2024 Nonlinear evolution of vortical disturbances entrained in the entrance region of a circular pipe. J. Fluid Mech. 998, A19.10.1017/jfm.2024.882CrossRefGoogle Scholar
Figure 0

Figure 3. Comparison between the original results (blue lines) and the corrected results (black lines). Only the nonlinear results are presented as the linear results are unaffected.

Figure 1

Figure 4. Comparison between the original results (blue lines) and the corrected results (black lines).

Figure 2

Figure 5. Comparison between the original results (blue lines) and the corrected results (black lines).

Figure 3

Figure 6. Comparison between the original results (blue lines) and the corrected results (black and red lines).

Figure 4

Figure 7. $(c)$ and $(d)$ Comparison between the original results (blue lines) and the corrected results (black lines).

Figure 5

Figure 16. Comparison of $(a)$ the mean flow and $(b)$ the perturbation flow between the experimental measurements (circles) and our numerical results (lines). Open and solid circles: experimental data measured by Wygnanski & Champagne (1973) (refer to as WC73 in the figure) with $(u_{rms}/\bar {U})_{cl}=5.8\,\%$ and $7.8\,\%$. Dotted and solid lines: present results with the new values $\epsilon =0.05$, $0.09$. The other parameters are unvaried: $Re_R=1200$, $x_R = 30$, $k_{x\kern-1pt,\kern-1pt R}=0.118$, $l=2$ and $m_0=2$.