1998
DOI: 10.1016/s0735-1933(98)00020-7
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The similarity of turbulent spots in subsonic boundary layers

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Cited by 3 publications
(5 citation statements)
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“…This increase appears to be consistent with the results of Zhong et al (2000), who also measured turbulent spots in water. However, this increase is lower than the peak heat transfer found by Clark et al (1994) and de Lange et al (1998), whose experiments in air measured spots with peak levels comparable to average levels in turbulent boundary layers. This discrepancy is probably a result of the difference in Prandtl numbers between the air and water experiments.…”
Section: Combined Flow Field and Surface Heat Transfer Datacontrasting
confidence: 57%
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“…This increase appears to be consistent with the results of Zhong et al (2000), who also measured turbulent spots in water. However, this increase is lower than the peak heat transfer found by Clark et al (1994) and de Lange et al (1998), whose experiments in air measured spots with peak levels comparable to average levels in turbulent boundary layers. This discrepancy is probably a result of the difference in Prandtl numbers between the air and water experiments.…”
Section: Combined Flow Field and Surface Heat Transfer Datacontrasting
confidence: 57%
“…Further, Clark et al (1994) and Ching & LaGraff (1995) also found that the peak heat transfer is between 0.48U ∞ and 0.56U ∞ , which is consistent with the peak at ξ ≈ 0.5 in figure 9. In contrast, the heat-transfer measurements of de Lange et al (1998) and Zhong et al (2000) imply the leading and trailing edges of the heat transfer coincide with the leading and trailing edges of the flow structures within the spot. However, Zhong et al (2000) reported the leading-edge speed of the heat-transfer fluctuations to be 0.78U ∞ and, when the data is replotted in similarity coordinates, the peak surface-heat transfer speed is in the range 0.5 < ξ < 0.6.…”
Section: Combined Flow Field and Surface Heat Transfer Datamentioning
confidence: 80%
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“…Despite a large scatter of the data a clear decrease of the lateral spreading with increasing Mach number was found. Measurements on naturally occurring turbulent spots in subsonic and supersonic boundary layers along flat plates were performed by Clark et al (1994), de Lange et al (1998 and Mee (2002). They detected turbulent spots and their growth from heat transfer measurements at the wall.…”
Section: Introductionmentioning
confidence: 99%