2004
DOI: 10.1017/s002211200300747x
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Intermittency, pressure and acceleration statistics from hot-wire measurements in wind-tunnel turbulence

Abstract: From hot-wire anemometer measurements in active-grid wind-tunnel turbulence we have determined the Reynolds number dependence of the velocity derivative moments, the mean-squared pressure gradient, χ, and the normalized acceleration variance, a 0 , over the Reynolds number range 100 6 R λ 6 900. The values of χ and a 0 were obtained from the fourth-order velocity structure functions. The derivative moments show power-law dependence on Reynolds number and the exponent is the same with or without shear. In parti… Show more

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Cited by 66 publications
(72 citation statements)
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“…Skewness S = γ 3 = −0.4 and kurtosis K = γ 4 = 20 were calculated. Wind-tunnel observations (Gylfason et al, 2004) suggest a power-law dependency of S and K on the Tay ≈ 28, which are in qualitative agreement with the directly calculated S and K. It has to be considered that the hot-wire measurements have a spatial resolution of about 10 · η and the smallest relevant scales cannot be resolved, which can explain the possible underestimation of S and K. In free-atmospheric clouds K ≈ 8 has been observed at scales ∼ 20 · η with strongly increasing values with increasing resolution (Siebert et al, 2010b).…”
Section: Hot-wire Measurements: Fine-scale Turbulencementioning
confidence: 99%
“…Skewness S = γ 3 = −0.4 and kurtosis K = γ 4 = 20 were calculated. Wind-tunnel observations (Gylfason et al, 2004) suggest a power-law dependency of S and K on the Tay ≈ 28, which are in qualitative agreement with the directly calculated S and K. It has to be considered that the hot-wire measurements have a spatial resolution of about 10 · η and the smallest relevant scales cannot be resolved, which can explain the possible underestimation of S and K. In free-atmospheric clouds K ≈ 8 has been observed at scales ∼ 20 · η with strongly increasing values with increasing resolution (Siebert et al, 2010b).…”
Section: Hot-wire Measurements: Fine-scale Turbulencementioning
confidence: 99%
“…Second, to our knowledge, there are no experimental or numerical data that directly address the conditional acceleration term of Eq. (9), though related conditional data are accumulating rapidly [17,18].…”
mentioning
confidence: 99%
“…For an incomplete list, see Ref. [18,20,21]. We compare in Table I the theoretical numbers above with the data of [21] in the atmospheric boundary layer at very high Reynolds numbers and the latest wind tunnel measurements [18] in grid turbulence.…”
mentioning
confidence: 99%
“…Specifically, they suggest that the flatness factor increases up to Re k = 700, but then decreases before eventually increasing again. However, the wind-tunnel experiments of [2] show no such transition. Direct numerical simulation (DNS) of turbulent flows has the potential to settle this argument because it is free from experimental ambiguities such as the effects of using Taylor's hypothesis, one-dimensional surrogates and so on.…”
Section: Introductionmentioning
confidence: 93%