Summary
Computer generated white noise sequences were used to excite a zero pressure gradient laminar boundary layer. This form of excitation generated modulated disturbance waves in a controlled and deterministic manner. By repeatedly exciting the flow with the same noise sequence, it was possible to examine the spatio-temporal evolution of the disturbance system with a single measurement probe. The development of the resulting flow structures immediately preceding the formation of a turbulent spot was investigated using hot-wire anemometry. The analysis of hot-wire measurements indicated that the resultant highly three-dimensional flow field was associated with the development of a horseshoe vortex in the flow.
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References
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Shaikh, F.N. and Gaster, M.: The non-linear evolution of modulated waves in a boundary layer. Journal of Eng. Math. 28, (1994) 55–71.
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© 1995 Springer-Verlag Berlin Heidelberg
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Shaikh, F.N., Gaster, M. (1995). The Natural Evolution of Turbulent Spots in a Flat Plate Laminar Boundary Layer. In: Kobayashi, R. (eds) Laminar-Turbulent Transition. IUTAM Symposia. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-79765-1_32
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DOI: https://doi.org/10.1007/978-3-642-79765-1_32
Publisher Name: Springer, Berlin, Heidelberg
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