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...
Hauptverfasser: | Walsh, E, Brighenti, F, Mceligot, D, ASME |
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Format: | Journal article |
Sprache: | English |
Veröffentlicht: |
2008
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