Experiments are described in which well-defined FSN (Free Stream Nonuniformity) distributions are introduced by placing fine wires upstream of the leading edge of a flat plate. Large amplitude spanwise thickness variations are present in the downstream boundary layer resulting from the interaction of the laminar wakes with the leading edge. Regions of elevated background unsteadiness appear on either side of the peak layer thickness, which share many of the characteristics of Klebanoff modes, observed at elevated Free Stream Turbulence (FST) levels. However, for the low background disturbance level of the free stream, the layer remains laminar to the end of the test section (Rx ≈ l.4×106) and there is no evidence of bursting or other phenomena associated with breakdown to turbulence. A vibrating ribbon apparatus is used to demonstrate that the deformation of the mean flow is responsible for substantial phase and amplitude distortion of Tollmien-Schlichting (TS) waves. Pseudo-flow visualization of hot-wire data shows that the breakdown of the distorted waves is more complex and occurs at a lower Reynolds number than the breakdown of the K-type secondary instability observed when the FSN is not present.
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ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference
July 6–10, 2003
Honolulu, Hawaii, USA
Conference Sponsors:
- Fluids Engineering Division
ISBN:
0-7918-3696-7
PROCEEDINGS PAPER
Effects of Weak Free Stream Nonuniformity on Boundary Layer Transition (Keynote Paper)
Jonathan H. Watmuff
Jonathan H. Watmuff
Royal Melbourne Institute of Technology, Melbourne, VIC, Australia
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Jonathan H. Watmuff
Royal Melbourne Institute of Technology, Melbourne, VIC, Australia
Paper No:
FEDSM2003-45685, pp. 1883-1892; 10 pages
Published Online:
February 4, 2009
Citation
Watmuff, JH. "Effects of Weak Free Stream Nonuniformity on Boundary Layer Transition (Keynote Paper)." Proceedings of the ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference. Volume 1: Fora, Parts A, B, C, and D. Honolulu, Hawaii, USA. July 6–10, 2003. pp. 1883-1892. ASME. https://doi.org/10.1115/FEDSM2003-45685
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