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Effect of high free-stream turbulence with large length scale on blade heat/mass transfer

Journal Article · · Journal of Turbomachinery
DOI:https://doi.org/10.1115/1.2841304· OSTI ID:351617
; ;  [1]
  1. Univ. of Minnesota, Minneapolis, MN (United States). Dept. of Mechanical Engineering

The naphthalene sublimation technique is used to investigate the influence of high free-stream turbulence with large length scale on the heat/mass transfer from a turbine blade in a highly accelerated linear cascade. The experiments are conducted at four exit Reynolds numbers, ranging from 2.4 {times} 10{sup 5} to 7.8 {times} 10{sup 5}, with free-stream turbulence of 3, 8.5, and 18% and corresponding integral length scales of 0.9 cm, 2.6 cm, and 8 cm, respectively. On the suction surface, the heat/mass transfer rate is significantly enhanced by high free-stream turbulence due to an early boundary layer transition. By contrast, the transition occurs very late, and may not occur at very low Reynolds numbers with low free-stream turbulence due to an early boundary layer transition. By contrast, the transition occurs very late, and may not occur at very low Reynolds numbers with low free-stream turbulence. In the turbulent boundary layer, lower heat/mass transfer rates are found for the highest free-stream turbulence level with large length scale than for the moderate turbulence levels with relatively small scales. Similar phenomena also occur at the leading edge. However, the effect of turbulence is not as pronounced in the laminar boundary layer.

Sponsoring Organization:
USDOE Morgantown Energy Technology Center, WV (United States)
DOE Contract Number:
FC21-92MC29061
OSTI ID:
351617
Report Number(s):
CONF-980615--
Journal Information:
Journal of Turbomachinery, Journal Name: Journal of Turbomachinery Journal Issue: 2 Vol. 121; ISSN JOTUEI; ISSN 0889-504X
Country of Publication:
United States
Language:
English

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