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Transition at Natural Conditions and Comparison with the Results of Wind Tunnel Studies

  • B. Yu. Zanin
Part of the International Union of Theoretical and Applied Mechanics book series (IUTAM)

Summary

The results of the experimental investigations of boundary-layer laminar-turbulent transition on the glider wing by hot-wire anemometer and sublimating coating films are presented. The comparison between the measurement results at flight and in the wind tunnel is conducted.

Keywords

Boundary Layer Wind Tunnel Free Flow Turbulence Level Tungsten Wire 
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References

  1. 1.
    Kachanov, Yu.S.; Kozlov, V.V.; Levchenko, V.Ya.: Beginning of turbulence in a boundary layer (in Russian). Novosibirsk: Nauka 1982.Google Scholar
  2. 2.
    Main-Smith, J.D.: Chemical solids as diffusible coating films for visual indications of boundary-layer transition in air and water. A.R.C., RM N°2755 (1950) 1745–1760.Google Scholar
  3. 3.
    Dovgal, A.V.; Kozlov, V.Y.: Influence of acoustic disturbances for structure in the boundary layer at unfavourable pressure gradient (in Russian). Izv. Akad. Nauk SSSR, Mekh. Zhidk. i Gaza 2 (1983) 48–52.Google Scholar

Copyright information

© Springer-Verlag, Berlin, Heidelberg 1985

Authors and Affiliations

  • B. Yu. Zanin
    • 1
  1. 1.Institute of Theoretical and Applied MechanicsSiberian Branch of the USSR Academy of SciencesNovosibirskUSSR

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