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The Predictions of Common Turbulence Models in a Mature Vortex

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Abstract

A range of turbulence models is exercised in the problem of a mature two-dimensional isolated vortex with high circulation Reynolds number, mature meaning that the core size has grown to many times its initial value, and the vortex reaches a self-similar state in which all quantities scale with its outside circulation Γ and its age t. The reasoning closely follows the landmark papers of Govindaraju and Saffman (Phys. Fluids 14, 2074–2080, 1971) (GS) and Zeman (Phys. Fluids A 7, 135–143, 1995), and we call this the GSZ flow. The models produce radically different outcomes, and this simple problem clearly places each model into one of two classes, in terms of its predictions in vortices. Some reach a turbulent state, including the circulation overshoot first predicted by GS, whereas others reach a laminar state free of overshoot. We have no evidence of non-unique solutions or bifurcations for a given model. The overshoot consists in the circulation, as a function of radius r, rising from zero on the axis at r = 0 to values that exceed the outside circulation Γ, and then falling back down. This happens within the turbulent region, and it is associated with the creation by turbulence of mean vorticity of sign opposite to the core vorticity. We consider the second (i.e., the laminar) response as the correct one, the circulation overshoot appearing to us unphysical, a thought which was clear in both of the original papers and is supported by experimental and simulation results. The laminar state is given by eddy-viscosity models only when they include a rotation/curvature correction. A Reynolds-stress transport model and an Explicit Algebraic Reynolds-Stress Model return turbulent solutions but with weak turbulence, which we consider a positive result, although Zeman’s Reynolds-stress model prevented any overshoot and led to a laminar mature flow. We believe this flow can become a relevant, well-defined, standard test case for turbulence models.

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References

  1. Chow, J.S., Zilliac, G.G., Bradshaw, P.: Mean and turbulence measurements in the near field of a Wingtip Vortex. AIAA J. 35(10), 1561–1567 (1997)

    Article  Google Scholar 

  2. Jacquin, L., Pantano, C.: On the persistence of trailing vortices. J. Fluid Mech. 471, 159–168 (2002)

    Article  MathSciNet  MATH  Google Scholar 

  3. Govindaraju, S., Saffman, P.: Flow in a turbulent trailing vortex. Phys. Fluids 14, 2074–2080 (1971)

    Article  Google Scholar 

  4. Rumsey, C.L.: NASA Langley Turbulence Modeling Resource, http://turbmodels.larc.nasa.gov/

  5. Dacles-Mariani, J., Zilliac, G.G., Chow, J.S., Bradshaw, P.: Numerical/experimental study of a Wingtip Vortex in the near field. AIAA J. 33(9), 1561–1568 (1995)

    Article  Google Scholar 

  6. Churchfield, M.J., Blaisdell, G.A.: Numerical simulations of a Wingtip Vortex in the near field. J. Aircr. 46(1), 230–243 (2009)

    Article  Google Scholar 

  7. Shur, M.L., Strelets, M.K., Travin, A.K., Spalart, P.R.: Turbulence modeling in rotating and curved channels: assessing the Spalart-Shur correction. AIAA J. 38(5), 784–792 (2000)

    Article  Google Scholar 

  8. Duraisamy, K., Lele, S.K.: Evolution of isolated, turbulent trailing vortices. Phys. Fluids 20, 3 (2008)

    Article  MATH  Google Scholar 

  9. Phillips, W.R.C., Graham, J.A.H.: Reynolds stress measurements in a turbulent trailing vortex. J. Fluid Mech. 147, 353–371 (1984)

    Article  Google Scholar 

  10. Williams, D.M., Kamenetskiy, D.S., Spalart, P.R.: On stagnation pressure increases in calorically perfect, ideal gases. Int. J. Heat Fluid Flow 58, 40–53 (2016)

    Article  Google Scholar 

  11. Spalart, P.R., Allmaras, S.R.: A one-equation turbulence model for aerodynamic flows. La Recherche Aerospatiale 1, 5–21 (1994)

    Google Scholar 

  12. Shur, M.L., Strelets, M.K., Travin, A.K.: High-order implicit multi-block Navier-Stokes code: ten-year experience of application to RANS/DES/LES/DNS of turbulence // https://cfd.spbstu.ru//agarbaruk/doc/NTS_code.pdf

  13. Rogers, S.E., Kwak, D.: An upwind differencing scheme for the incompressible Navier-Stokes equations. Appl. Num. Math. 8, 43–64 (1991)

    Article  MathSciNet  MATH  Google Scholar 

  14. Menter, F.R.: Two-equation Eddy-viscosity turbulence models for engineering applications. AIAA J. 32(8), 1598–1605 (1994)

    Article  Google Scholar 

  15. Smirnov, P.E., Menter, F.R.: Sensitization of the SST turbulence model to rotation and curvature by applying the Spalart-Shur correction term. ASME J. Turbomach. 131 (2009)

  16. Speziale, C.G., Sarkar, S., Gatski, T.B.: Modelling the pressure–strain correlation of turbulence: an invariant dynamical systems approach. J. Fluid Mech. 227 (6), 245–272 (1991)

    Article  MATH  Google Scholar 

  17. Cecora, R.D., Radespiel, R., Eisfeld, B., Probst, S.: Differential Reynolds stress modeling for aeronautics. AIAA J. 53, 739–755 (2015)

    Article  Google Scholar 

  18. Wallin, S., Johansson, A.V.: An explicit algebraic reynolds stress model for incompressible and compressible turbulent flows. J. Fluid Mech. 403(2000), 89–132 (2000)

    Article  MathSciNet  MATH  Google Scholar 

  19. Menter, F.R., Garbaruk, A.V., Egorov, Y.: Explicit algebraic reynolds stress models for anisotropic wall-bounded flows. In: Proceedings of the EUCASS—3rd European Conference for Aero-Space Sciences (2009)

  20. Zeman, O.: The persistence of trailing vortices: a modeling study. Phys. Fluids A 7, 135–143 (1995)

    Article  MATH  Google Scholar 

  21. Wallin, S., Johansson, A.V.: Modelling streamline curvature effects in explicit algebraic Reynolds stress turbulence models. Int. J. Heat Fluid Flow 23(5), 721–730 (2002)

    Article  Google Scholar 

  22. Hoffman, E.R., Joubert, P.N.: Turbulent line vortices. J. Fluid Mech. 16, 395–411 (1963)

    Article  MATH  Google Scholar 

  23. Spalart, P.R.: On the motion of laminar wing wakes in a stratified fluid. J. Fluid Mech. 327, 139–160 (1996)

    Article  MATH  Google Scholar 

Download references

Acknowledgments

The results of the work were obtained using computational resources of Peter the Great Saint-Petersburg Polytechnic University Supercomputing Center (http://www.spbstu.ru). Prof. G. Huang contributed numerical results and valuable discussions, and Dr. M. Churchfield reviewed the manuscript in detail.

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Correspondence to Philippe R. Spalart.

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Appendix

Appendix

The analysis of the laminar-turbulent interface for the GSZ flow and the Spalart-Allmaras model is as follows. It involves the velocity u𝜃(r, t) and the eddy viscosity νt(r, t), the momentum equation introduced above

$$r^{2}\frac{\partial u_{\theta } }{\partial t}=\frac{\partial }{\partial r}\left[ {r^{2}\nu_{t} \left( {\frac{\partial u_{\theta } }{\partial r}-\frac{u_{\theta } }{r}} \right)} \right] $$

and the model equation ([4], with the passive terms removed)

$$\frac{\partial \nu_{t} }{\partial t}=c_{b1} \left| \omega \right|\nu_{t} +\frac{1}{\sigma }\left[ {\frac{1}{r}\frac{\partial }{\partial r}\left( {r\nu_{t} \frac{\partial \nu_{t} }{\partial r}} \right)+c_{b2} \left( {\frac{\partial \nu_{t} }{\partial r}} \right)^{2}} \right] $$

The interface is propagating at a velocity c = dr1/dt, so that to leading order a time derivative such as \(\frac {\partial \nu _{t} }{\partial t}\) is equal to \(-c\frac {\partial \nu _{t} }{\partial r}\). We assume that both the deviation from an irrotational vortex field, u𝜃 −Γ/(2πr), and the eddy viscosity νt, approach zero at r = r1 linearly (write u𝜃 −Γ/(2πr) = A (r1r) and νt = B (r1r)). Thus, \(\frac {\partial \nu _{t} }{\partial t}=cB\). The slopes A and B of these functions introduce two more unknowns besides c.

Once these distributions are introduced into the governing equations, the production (cb1) term vanishes at r = r1, and the model equation only involves the time derivative and diffusion terms much like in the original SA paper [11]. Then, both c and B drop out of the equations, which produces A as a function of Γ, r1, and the model constants.

$$A=\frac{\sigma }{1+c_{b2} -\sigma }\frac{{\Gamma} }{\pi {r_{1}^{2}} } $$

The vorticity is actually –A.

$$\omega =\frac{1}{r}\frac{\partial \left( {r u_{\theta }} \right)}{\partial r} =-\frac{\sigma }{1+c_{b2} -\sigma }\frac{{\Gamma} }{\pi{r_{1}^{2}} } $$

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Spalart, P.R., Garbaruk, A.V. The Predictions of Common Turbulence Models in a Mature Vortex. Flow Turbulence Combust 102, 667–677 (2019). https://doi.org/10.1007/s10494-018-9983-6

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