EVOLUTION OF THE LAMINAR BOUNDARY LAYER OVER A FLAT PLATE UNDER A FREE STREAM TURBULENCE INTENSITY OF 1.3%
The evolution of the laminar boundary layer over a flat plate under a free stream turbulence intensity of 1.3% is analysed. The effect of free stream turbulence on the onset of transition is one of the important sources leading to bypass transition. Such disturbances are of great interest in enginee...
Main Authors: | Walsh, E, Brighenti, F, Mceligot, D, ASME |
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Format: | Journal article |
Language: | English |
Published: |
2008
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