2005
DOI: 10.1115/1.1861920
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Effect of Elevated Free-Stream Turbulence on Transitional Flow Heat Transfer Over Dual-Scaled Rough Surfaces

Abstract: The surface roughness over a serviced turbine airfoil is usually multiscaled with varying features that are difficult to be universally characterized. However, it was previously discovered in low free-stream turbulence conditions that the height of larger roughness produces separation and vortex shedding, which trigger early transition and exert a dominant effect on flow pattern and heat transfer. The geometry of the roughness and smaller roughness scales played secondary roles. This paper extends the previous… Show more

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Cited by 5 publications
(2 citation statements)
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“…The introduction of free-stream turbulence over a rough surface resulted in even greater increases in heat transfer (~100%). Similar results were seen by Wang and Rice [94], Turner et al [65] and Bons [59] when increasing turbulence intensity over a rough surface. These studies also showed that the effects of surface roughness and turbulence intensity on heat transfer seemed to be roughly cumulative.…”
Section: Roughness Effects On Convective Heat Transfer In Cfr Enginesupporting
confidence: 77%
“…The introduction of free-stream turbulence over a rough surface resulted in even greater increases in heat transfer (~100%). Similar results were seen by Wang and Rice [94], Turner et al [65] and Bons [59] when increasing turbulence intensity over a rough surface. These studies also showed that the effects of surface roughness and turbulence intensity on heat transfer seemed to be roughly cumulative.…”
Section: Roughness Effects On Convective Heat Transfer In Cfr Enginesupporting
confidence: 77%
“…from available experiments as a function of wall roughness expressed by the ratio k s / at the rough strip end. This difference represents the correction of the criterion for the transition onset.The estimation of this relation was derived using experimental data of Pinson and Wang[21] and Wang and Rice[22] related to the transition on the flat plate with smooth and/or rough walls. Further results of the investigation of flow over the airfoil NACA0012 with a rough strip downstream of the leading edge according to Kerho and Bragg[23] were used.…”
mentioning
confidence: 99%