2022
DOI: 10.1017/jfm.2022.156
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Study of a rough-wall turbulent boundary layer under pressure gradient

Abstract: The behaviour of a fully rough-wall turbulent boundary layer subjected to different pressure gradients is investigated for different Reynolds numbers using hot-wire measurements. Mean velocity and velocity root-mean-square measurements indicate that the boundary layer remains in a self-preserving state regardless of the pressure gradient. However, different pressure gradients lead to different self-preservation states, as suggested by the lack of collapse of the velocity profile between the pressure gradient c… Show more

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Cited by 4 publications
(2 citation statements)
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“…• Roughness elements small compared to the viscous sublayer thickness (hydraulically smooth); • Roughness elements in the same order of thickness as the viscous sublayer thickness (transitionally rough); and • Roughness elements larger than the viscous sublayer thickness and ending inside the buffer or the logarithmic layer (fully rough) [10]. The roughness effect of the flow field is no more limited to the viscous sublayer [66]. 𝑘 , and 𝑘 , delimit the regimes and take different values depending on the type of roughness encountered.…”
Section: The Rough Flow Regimesmentioning
confidence: 99%
“…• Roughness elements small compared to the viscous sublayer thickness (hydraulically smooth); • Roughness elements in the same order of thickness as the viscous sublayer thickness (transitionally rough); and • Roughness elements larger than the viscous sublayer thickness and ending inside the buffer or the logarithmic layer (fully rough) [10]. The roughness effect of the flow field is no more limited to the viscous sublayer [66]. 𝑘 , and 𝑘 , delimit the regimes and take different values depending on the type of roughness encountered.…”
Section: The Rough Flow Regimesmentioning
confidence: 99%
“…The large scatter of the reported AEP losses is partly due to the fact that this quantity depends on the specific geometry of the blade surface perturbation As erosion progresses and the perturbations of the LE geometry approach or exceed the BL thickness, additional aerodynamic losses occur, which may vary significantly with the specific LEE damage [15]. These phenomena contribute, with strength depending on the erosion severity, to premature separation of the BL on the airfoil upper side at AoAs where the nominal airfoil has a clean flow [7,16,17], with consequent reduction of the lift and further increase of the drag.…”
Section: Introductionmentioning
confidence: 99%