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.
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References
Kachanov, Yu.S.; Kozlov, V.V.; Levchenko, V.Ya.: Beginning of turbulence in a boundary layer (in Russian). Novosibirsk: Nauka 1982.
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.
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.
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© 1985 Springer-Verlag, Berlin, Heidelberg
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Zanin, B.Y. (1985). Transition at Natural Conditions and Comparison with the Results of Wind Tunnel Studies. In: Kozlov, V.V. (eds) Laminar-Turbulent Transition. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-82462-3_67
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DOI: https://doi.org/10.1007/978-3-642-82462-3_67
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-82464-7
Online ISBN: 978-3-642-82462-3
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