One-dimensional turbulence investigation of variable density effects due to heat transfer in a low Mach number internal air flow

https://doi.org/10.1016/j.ijheatfluidflow.2019.108481Get rights and content

Highlights

  • We introduce an extension of the spatial ODT formulation (S-ODT), in order to study a variable density internal air flow.

  • S-ODT results are compared to the results of a traditional temporal ODT formulation (T-ODT) and to reference DNS data.

  • For bulk quantities, both the T-ODT and S-ODT formulations have a similar performance in comparison to DNSs.

  • For the evaluation of radial distributions, the S-ODT formulation clearly outperforms the T-ODT formulation.

Abstract

A novel spatial formulation of the One-Dimensional Turbulence (ODT) model is applied to a vertical pipe-flow with heat transfer, analogous to the Direct Numerical Simulation (DNS) performed by Bae et al. [Phys. Fluids 18, (075102) (2006)]. The framework presented here is an extension for radially confined domains of the cylindrical ODT spatial formulation for low Mach number flows with variable density. The variable density simulations for air (Prandtl number Pr=0.71) are performed at an initial bulk Reynolds number Reb,0,DNS=6000 and Grashof number Gr0,DNS=6.78×106. ODT results are presented for both the spatial formulation introduced in this work and the standard temporal formulation for cylindrical flows introduced by Lignell et al. [Theor. Comput. Fluid Dyn. 32, 4 (2018), pp. 495–20]. Streamwise bulk profiles and radial profiles at specific streamwise positions for the temporal and spatial formulations are in good agreement with the DNS results from Bae et al. For the present application, the spatial formulation yields physically better results in comparison to the temporal formulation. Overall, the findings in the original work of Bae et al. were corroborated with ODT. Although the framework proposed in this work is not a compressible framework and has some clear limitations regarding conservation properties, we suggest its use for future studies in the low Mach number variable density regime.

Introduction

Some understanding of the physics associated with the thermal boundary layers in wall-bounded flows with adverse pressure gradients has been achieved parallel to the increase in the number of heat transfer applications for pipes (Van Driest, 1956, McEligot, Coon, Perkins, 1970, Huang, Coleman, Bradshaw, 1995). Although it is tempting to think about compressible flow whenever analyzing variable density effects, there is a large number of everyday applications involving variable density, which do not necessarily deal with the intrincate phenomena happening at elevated velocity (high Mach number), e.g. heating or cooling, as well as some geophysical applications (Davidson, 2013). In comparison, however, to the research on incompressible pipe-flow in Direct Numerical Simulations (DNSs) (Satake, Kunugi, Himeno, 2000, Wu, Moin, 2008, Chin, Monty, Ooi, 2014, Ahn, Lee, Lee, Kang, Sung, 2015), only few studies have tackled pipe-flow problems with variable properties (Bae, Yoo, Choi, 2005, Xu, Lee, Pletcher, 2005, Bae, Yoo, Choi, McEligot, 2006, Ghosh, Foysi, Friedrich, 2010, Modesti, Pirozzoli, 2019). Bae et al. discussed the dissimilar behavior between the velocity and temperature profiles in a low Mach number internal air flow with large temperature gradients (Bae et al., 2006). Turbulence statistics from compressible and incompressible pipe and channel flow were also studied up to a second-order degree in the work done by Ghosh et al. (2010). Nonetheless, and due to practical reasons, the detailed numerical simulations with variable properties remain restricted to relatively low Reynolds numbers (e.g. up to Reb=31500, as in Modesti and Pirozzoli (2019)).

In order to simulate flows at large Reynolds numbers, a large family of turbulence models have been formulated. In the field of map-based stochastic turbulence models, Alan Kerstein proposed in 1999 the idea of One-Dimensional Turbulence (ODT) (Kerstein, 1999). Much of the research effort in ODT has been devoted to free shear and wall-bounded flows. As first formal applications in this context, Dreeben and Kerstein investigated the problem of stationary buoyant turbulent flow in a vertical slot using an incompressible formulation and a Boussinesq approach (Dreeben and Kerstein, 2000). Likewise, Echekki et al. (2001) presented a framework for the evaluation of stationary spatially developing jets on the basis of temporally evolving jets, where heat and mass transfer were evaluated in the context of a jet diffusion flame. Ashurst and Kerstein were the first ones to present a framework for variable density treatment in ODT. They also introduced an extension for spatially developing free shear flows with variable density, which did not require a temporal-to-spatial transformation (Ashurst and Kerstein, 2005). Recently, a novel cylindrical extension of ODT was formulated by Lignell et al. (2018). As in Ashurst and Kerstein (2005), the spatial formulation from Lignell et al. (2018) is limited to free shear flows, such as jets, which have a mathematical description portraying a parabolic behaviour in nature, in the light of the low Mach number approximation. Therefore, in order to partially overcome the constraints associated with the traditional spatial ODT formulation, we seek an extension of the formulation for wall-bounded flows with variable properties within the low Mach number approximation.

This paper is structured as follows: in Section 2 we discuss the low Mach number treatment of the deterministic ODT part for the temporal and spatial formulations, as well as the stochastic turbulent advection treatment. Section 3 discusses the initial conditions of the simulation setup and presents the results for bulk quantities, velocity and temperature distributions, as well as their turbulent fluctuations. In Section 4, we summarize and conclude our findings. As a complement to the work, theoretical considerations regarding the chosen form of the shear stress tensor for the cylindrical formulation are given in Appendix A. Details of the numerical procedure are given in Appendix C, while a discussion about statistical quantities in ODT for the variable density formulation are given in Appendix D.

Section snippets

ODT model formulation

Fig. 1 shows two canonical flow configurations with cylindrical geometry for a radially open and confined domain, respectively. The round jet case shown in Fig. 1(a) is an example for an open domain flow. This case can be simulated with the cylindrical ODT formulation of Lignell et al. (2018). It is addressed here only for comparison. The flow leaves a circular nozzle (radius R) and evolves in positive z-direction due to turbulent break-up and diffusion. The flow domain of interest is a

Strongly heated variable density simulations

We now discuss the results obtained with the variable density T-ODT and S-ODT formulations in a large heat transfer regime. The ODT simulations aim to replicate the results from Bae et al. (2006), where a strongly heated air flows from the bottom to the top of a vertical pipe. Gravity effects are considered here. The simulations are based on the case 618 from Bae et al. (2006). Air, as an ideal gas mixture (21% O2 and 79% N2, Pr=0.71), is considered for all the simulations. NASA polynomials

Conclusions

A novel spatial ODT formulation (S-ODT) for internal air flows (radially confined ODT domains) with variable density regimes has been developed and validated in this paper. This S-ODT formulation is complementary to the previous S-ODT formulation presented in Lignell et al. (2018), which is mainly applicable for open domain configurations. The formulation presented here is, however, not a compressible formulation, and its main purpose is to account for variable inertia effects in low Mach

Funding

The authors would like to acknowledge the financial support from the European Regional Development Fund (EFRE-Brandenburg). This work was carried out within the framework of the project ’Einsatz elektrohydrodynamisch getriebener Strömungen zur erweiterten Nutzung von Elektroabscheidern’, grant number StaF 23035000.

Declaration of Competing Interest

None.

Acknowledgements

The authors would also like to thank and acknowledge the support of the Norddeutsche Verbund für Hoch- und Höchstleistungsrechnen (HLRN - Berlin, Germany) for the supply of the computational resources. Last but not least, we thank the reviewers of the manuscript for their constructive criticism which helped to improve the consistency of the model formulation.

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