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Coherent turbulence and entrainment in a supersonic, axisymmetric, separated/reattaching shear layer

Branden M. Kirchner*, Gregory S. Elliott, and J. Craig Dutton

  • University of Illinois at Urbana-Champaign, Department of Aerospace Engineering, Urbana, Illinois, USA

  • *kirchnr2@gmail.com
  • elliottg@illinois.edu
  • jcdutton@illinois.edu

Phys. Rev. Fluids 5, 084605 – Published 10 August, 2020

DOI: https://doi.org/10.1103/PhysRevFluids.5.084605

Abstract

The influence of coherent turbulent structures on the entrainment characteristics of a separated shear layer in a Mach-2.49 longitudinal cylinder wake is investigated using stereoscopic particle image velocimetry (SPIV). Three thousand non-time-correlated velocity field measurements, acquired along a plane coincident with the central axis, were decomposed into modes using the snapshot proper orthogonal decomposition (POD) method. The second and third POD modes identified high-energy velocity fluctuations aligned with consistent directions in the separated shear layers, near the boundaries of the recirculation region. Previous work by the authors has demonstrated, using tomographic PIV, that these directionally consistent velocity fluctuations identified by the POD modes are caused by three-dimensional (3D) coherent upright and inverted hairpin vortex structures in this flow. The SPIV velocity field snapshots were conditionally sorted based on the value of their corresponding POD amplitude coefficients, and conditional statistics from these subsets of snapshots were used to derive results in the current work. It is demonstrated that a higher statistical prevalence of upright hairpin vortices in the shear layer directly correlates with reduced shear layer growth rates, and a subsequent increase in the reattachment length. Conversely, a higher statistical prevalence of inverted hairpin vortices correlates with increased shear layer growth rates, and a subsequent reduction in the reattachment length. Comparisons of conditional statistics for the SPIV data are drawn with previous laser Doppler velocimetry measurements acquired in a 5 boat-tailed cylinder configuration of this flow. These comparisons demonstrate clear similarities of important features between the two flows, such as an increase in the reattachment length when compared to the unconditional blunt-based cylinder flow, which is indicative of higher cylinder base pressures and subsequently reduced pressure drag.

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References (49)

  1. V. A. Amatucci, J. C. Dutton, D. W. Kuntz, and A. L. Addy, Two-stream, supersonic, wake flowfield behind a thick base, part I: General features, AIAA J. 30, 2039 (1992).
  2. F. Scarano and B. W. van Oudheusden, Planar velocity measurements of a two-dimensional compressible wake, Exp. Fluids 34, 430 (2003).
  3. R. Humble, F. Scarano, and B. W. van Oudheusden, Unsteady flow organization of compressible planar base flows, Phys. Fluids 19, 076101 (2007).
  4. B. M. Kirchner, J. V. Favale, G. S. Elliott, and J. C. Dutton, Three-component turbulence measurements and analysis of a supersonic, axisymmetric base flow, AIAA J. 57, 2496 (2019).
  5. C. Bourdon and J. C. Dutton, Planar visualizations of large-scale turbulent structures in axisymmetric supersonic separated flows, Phys. Fluids 11, 201 (1999).
  6. R. D. Sandberg, Numerical investigation of turbulent supersonic axisymmetric wakes, J. Fluid Mech. 702, 488 (2012).
  7. G. L. Brown and A. Roshko, On density effects and large structure in turbulent mixing layers, J. Fluid Mech. 64, 774 (1974).
  8. R. D. Sandberg and H. F. Fasel, Numerical investigation of transitional supersonic axisymmetric wakes, J. Fluid Mech. 563, 1 (2006).
  9. F. Simon, S. Deck, P. Guillen, P. Sagaut, and A. Merlen, Numerical simulation of the compressible mixing layer past an axisymmetric trailing edge, J. Fluid Mech. 591, 215 (2007).
  10. N. T. Clemens and M. G. Mungal, Large-scale structure and entrainment in the supersonic mixing layer, J. Fluid Mech. 284, 171 (1995).
  11. L. Rollstin, Measurement of inflight base-pressure on an artillery-fired projectile, in Atmospheric Flight Mechanics Conference (AIAA, Monterey, CA, 1987), pp. 195–201.
  12. J. L. Herrin and J. C. Dutton, Supersonic base flow experiments in the near wake of a cylindrical afterbody, AIAA J. 32, 77 (1994).
  13. S. B. Pope, The evolution of surfaces in turbulence, Int. J. Eng. Sci. 26, 445 (1988).
  14. J. Westerweel, C. Fukushima, J. M. Pedersen, and J. C. R. Hunt, Mechanics of the Turbulent-Nonturbulent Interface of a Jet, Phys. Rev. Lett. 95, 174501 (2005).
  15. J. Westerweel, C. Fukushima, J. M. Pedersen, and J. C. R. Hunt, Momentum and scalar transport at the turbulent/non-turbulent interface of a jet, J. Fluid Mech. 631, 199 (2009).
  16. J. L. Herrin and J. C. Dutton, Supersonic near-wake afterbody boattailing effects on axisymmetric bodies, J. Spacecr. Rockets 31, 1021 (1994).
  17. J. L. Herrin and J. C. Dutton, Effect of a rapid expansion on the development of compressible free shear layers, Phys. Fluids 7, 159 (1995).
  18. J. L. Herrin and J. C. Dutton, The turbulence structure of a reattaching axisymmetric compressible free shear layer, Phys. Fluids 9, 3502 (1997).
  19. L. Sirovich, Turbulence and the dynamics of coherent structures part 1: Coherent structures, Q. Appl. Math. 45, 561 (1987).
  20. P. E. Dimotakis, Two-dimensional shear layer entrainment, AIAA J. 24, 1791 (1986).
  21. R. Jahanbakhshi and C. K. Madnia, Entrainment in a compressible turbulent shear layer, J. Fluid Mech. 797, 564 (2016).
  22. S. Piponniau, E. Collin, P. Dupont, and J. F. Debiéve, Reconstruction of velocity fields from wall pressure measurements in a shock wave/turbulent boundary layer interaction, Int. J. Heat Fluid Flow 35, 176 (2012).
  23. D. Estruch-Samper and G. Chandola, Separated shear layer effect on shock-wave/turbulent-boundary-layer interaction unsteadiness, J. Fluid Mech. 848, 154 (2018).
  24. S. Kawai and K. Fujii, Computational study of a supersonic base flow using hybrid turbulence methodology, AIAA J. 43, 1265 (2005).
  25. M. Samimy and S. K. Lele, Motion of particles with inertia in a compressible free shear layer, Phys. Fluids 3, 1915 (1991).
  26. J. R. Janssen and J. C. Dutton, Time-series analysis of supersonic base-pressure fluctuations, AIAA J. 42, 605 (2004).
  27. G. Berkooz, P. Holmes, and J. L. Lumley, The proper orthogonal decomposition in the analysis of turbulent flows, Annu. Rev. Fluid Mech. 25, 539 (1993).
  28. P. L. van Gent, B. W. van Oudheusden, and F. F. J. Schrijer, Determination of mean pressure from PIV in compressible flows using the Reynolds-averaging approach, Exp. Fluids 59, 1 (2018).
  29. K. E. Meyer, J. M. Pedersen, and O. Ozcan, A turbulent jet in crossflow analysed with proper orthogonal decomposition, J. Fluid Mech. 583, 199 (2007).
  30. F. Stella, N. Mazellier, P. Joseph, and A. Kourta, Scaling of separated shear layers: An investigation of mass entrainment, J. Fluid Mech. 826, 851 (2017).
  31. K. U. Kim, G. S. Elliott, and J. C. Dutton, Three-dimensional experimental study of compressibility effects on turbulent free shear layers, AIAA J. 58, 133 (2020).
  32. P. Bradshaw, The effect of mean compression or dilatation on the turbulence structure of supersonic boundary layers, J. Fluid Mech. 63, 449 (1974).
  33. A. J. Smits, J. A. Eaton, and P. Bradshaw, The effect of short regions of high surface curvature on turbulent boundary layers, J. Fluid Mech. 94, 209 (1979).
  34. A. J. Smits and D. H. Wood, The response of turbulent boundary layers to sudden perturbations, Annu. Rev. Fluid Mech. 17, 321 (1985).
  35. B. M. Kirchner, G. S. Elliott, and J. C. Dutton, Hairpin vortex structures in a supersonic, separated, longitudinal cylinder wake, Phys. Fluids 32, 046103 (2020).
  36. D. Papamoschou and A. Roshko, The compressible turbulent shear layer: An experimental study, J. Fluid Mech. 197, 453 (1988).
  37. B. Knight and L. Sirovich, Kolmogorov Inertial Range for Inhomogeneous Turbulent Flows, Phys. Rev. Lett. 65, 1356 (1990).
  38. P. Das and A. De, Numerical investigation of flow structures around a cylindrical afterbody under supersonic conditions, Aerospace Sci. Technol. 47, 195 (2015).
  39. J. M. Wallace, H. Eckelmann, and R. S. Brodkey, The wall region in turbulent shear flow, J. Fluid Mech. 54, 39 (1972).
  40. M. Sieber, C. O. Paschereit, and K. Oberleithner, Spectral proper orthogonal decomposition, J. Fluid Mech. 792, 798 (2016).
  41. A. Towne, O. T. Schmidt, and T. Colonius, Spectral proper orthogonal decomposition and its relationship to dynamic mode decomposition and resolvent analysis, J. Fluid Mech. 847, 821 (2018).
  42. K. Taira, S. L. Brunton, S. T. M. Dawson, C. W. Rowley, T. Colonius, B. J. McKeon, O. T. Schmidt, S. Gordeyev, V. Theofilis, and L. S. Ukeiley, Modal analysis of fluid flows: An overview, AIAA J. 55, 4013 (2017).
  43. M. A. Mendez, M. Balabane, and J. M. Buchlin, Multi-scale proper orthogonal decomposition of complex fluid flows, J. Fluid Mech. 870, 988 (2019).
  44. C. W. Rowley and T. M. Dawson, Model reduction for flow analysis and control, Annu. Rev. Fluid Mech. 49, 387 (2017).
  45. R. J. Adrian, B. G. Jones, M. K. Chung, Y. Hassan, C. K. Nithianandan, and A. T. C. Tung, Approximation of turbulent conditional averages by stochastic estimation, Phys. Fluids A 1, 992 (1989).
  46. R. J. Adrian, Hairpin vortex organization in wall turbulence, Phys. Fluids 19, 041301 (2007).
  47. G. E. Elsinga, R. J. Adrian, B. W. Van Oudheusden, and F. Scarano, Three-dimensional vortex organization in a high-Reynolds-number supersonic turbulent boundary layer, J. Fluid Mech. 644, 35 (2010).
  48. S. Ghaemi and F. Scarano, Counter-hairpin vortices in the turbulent wake of a sharp trailing edge, J. Fluid Mech. 689, 317 (2011).
  49. J. Zhou, R. J. Adrian, S. Balachandar, and T. M. Kendall, Mechanisms for generating coherent packets of hairpin vortices in channel flow, J. Fluid Mech. 387, 353 (1999).

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