The influence of free stream turbulence intensity on boundary layer transition was studied for a weakly compressible flow along a flat plate. The test facility consisted of a Ludwieg tube in which values of Mach number, Reynolds number and free stream turbulence could be varied over the following ranges: 0.09 < M < 0.6, 5.105 < Reu/m < 1.107, 1.2% < Tu < 9%. In this paper the turbulence intensity was varied up to 4.0 %. Unsteady heat flux to the flat plate was measured using cold thin film gauges. From these measurements, the intermittency was computed using an integral technique. For turbulence intensities of 1.2 %, the intermittency distribution is somewhat below the Narasimha and Johnson model, whereas a good agreement is obtained for a free stream turbulence intensity of 4.0 %. The calculated dimensionless spot production rates is proved to agree very well with existing data sets from other experiments. For a Mach number equal to 0.36 the production rates seems a bit higher when compared to the incompressible data. However, the differences are small.
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ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7868-2
PROCEEDINGS PAPER
Influence of Turbulence Intensity on Intermittency Model in By-Pass Transition
C. J. Hogendoorn,
C. J. Hogendoorn
Eindhoven University of Technology, Eindhoven, The Netherlands
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H. C. de Lange,
H. C. de Lange
Eindhoven University of Technology, Eindhoven, The Netherlands
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A. A. van Steenhoven,
A. A. van Steenhoven
Eindhoven University of Technology, Eindhoven, The Netherlands
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M. E. H. van Dongen
M. E. H. van Dongen
Eindhoven University of Technology, Eindhoven, The Netherlands
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C. J. Hogendoorn
Eindhoven University of Technology, Eindhoven, The Netherlands
H. C. de Lange
Eindhoven University of Technology, Eindhoven, The Netherlands
A. A. van Steenhoven
Eindhoven University of Technology, Eindhoven, The Netherlands
M. E. H. van Dongen
Eindhoven University of Technology, Eindhoven, The Netherlands
Paper No:
97-GT-473, V001T03A089; 9 pages
Published Online:
December 24, 2014
Citation
Hogendoorn, CJ, de Lange, HC, van Steenhoven, AA, & van Dongen, MEH. "Influence of Turbulence Intensity on Intermittency Model in By-Pass Transition." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. Orlando, Florida, USA. June 2–5, 1997. V001T03A089. ASME. https://doi.org/10.1115/97-GT-473
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