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Hot-wire visualization of breakdown to turbulence in complex flows

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Thermophysics and Aeromechanics Aims and scope

Abstract

The nonlinear stage of breakdown to turbulence is a strongly three-dimensional process and represents a difficult task for experimental studies. Investigation of laminar-turbulent transition in aerospace applications additionally involves a complex base-flow with pressure gradients and secondary velocity components resulting in successive increase of necessary measurements. The developed hot-wire visualization technique offers a possibility for an advanced analysis whilst retaining the advantages of traditional visualization methods and is especially suitable for resolving such complex flows.

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References

  1. H.L. Reed and W.S. Saric, Stability of three-dimensional boundary layers, Annu. Rev. Fluid Mech., 1989, Vol. 21, P. 235–284.

    Article  MATH  MathSciNet  ADS  Google Scholar 

  2. P.S. Klebanoff, K.D. Tidstrom, and L.M. Sargent, The three-dimensional nature of boundary layer instability, J. Fluid Mech., 1962, Vol. 12, P. 1–34.

    Article  MATH  ADS  Google Scholar 

  3. Y.S. Kachanov, V.V. Kozlov, and V.Ya. Levchenko, Nonlinear development of a wave in a boundary layer, Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, 1977, Vol. 5, P. 85–94 (in Russian). Transl. Fluid. Dyn., 1978, Vol. 12, P. 383–390.

    Google Scholar 

  4. W. Saric, V. Kozlov, and V. Levchenko, Forced and unforced subharmonic resonance in boundary layer transition, AIAA Paper No. 84-0007, 1984.

  5. V.G. Chernoray, A.A. Bakchinov, V.V. Kozlov, and L. Loefdahl, Experimental study of the K-regime of breakdown in straight and swept wing boundary layers, Phys. Fluids, 2001, Vol. 13, No. 7, P. 2129–2132.

    Article  ADS  Google Scholar 

  6. V.G. Chernoray, A.V. Dovgal, V.V. Kozlov, and L. Loefdahl, Experiments on secondary instability of streamwise vortices in a swept wing boundary layer, J. Fluid Mech., 2005, Vol. 534, P. 295–325.

    Article  MATH  ADS  Google Scholar 

  7. S. Bake, D.G.W. Meyer, and U. Rist, Turbulence mechanism in Klebanoff transition: a quantitative comparison of experiment and direct numerical simulation. Ibid., 2002, Vol. 459, P. 217–243.

    Article  MATH  ADS  Google Scholar 

  8. Yu.A. Litvinenko, G.R. Grek, V.V. Kozlov, L. Loefdahl, and V.G. Chernoray, Experimental investigation of a streaky structure varicose instability in a swept wing boundary layer, Thermophysics and Aeromechanics, 2004, Vol. 11, No. 1, P. 13–21.

    Google Scholar 

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Thanks are due to the Royal Swedish Academy of Sciences, the Swedish Energy Agency (Energimyndigheten). The work was financially supported by the President of the Russian Federation (Grant No. NSh-964.2003.1), the Russian Foundation for Basic Research (Grant No. 05-01-00034) and Ministry of Education and Sciences of the Russian Federation (Grant No. RNP.2.1.2.3370).

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Chernoray, V.G., Kozlov, V.V., Loefdahl, L. et al. Hot-wire visualization of breakdown to turbulence in complex flows. Thermophys. Aeromech. 13, 213–220 (2006). https://doi.org/10.1134/10.1134/S0869864306020053

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  • DOI: https://doi.org/10.1134/10.1134/S0869864306020053

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