2017
DOI: 10.1063/1.4984243
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Experimental investigation on the unsteady lift of an airfoil in a sinusoidal streamwise gust

Abstract: The unsteady lift of a stationary airfoil encountering a sinusoidal streamwise gust is experimentally investigated under attached flow conditions. The airfoil has an NACA 0015 profile with a chord length c = 0.5 m. The Reynolds number of the main flow is in the range of 198 000 ⩽ Re ⩽ 331 000. The reduced frequency of the perturbation ω ranges from 0.047 to 0.392. The results show that the fluctuation in the lift force reduces very much at the high frequency. It can be attributed to a significant reduction in … Show more

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Cited by 63 publications
(12 citation statements)
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“…In this study, the unsteady lift on an oscillating airfoil encountering a sinusoidal streamwise gust is investigated using a multiple-fan actively controlled wind tunnel. The quality of the generated fluctuating flow was proved to be excellent (Yang et al 2017). The surface pressures of the airfoil are measured using DMS-4000 pressure scanners, and thus the lift force can be obtained by integration along the chord length of the airfoil.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…In this study, the unsteady lift on an oscillating airfoil encountering a sinusoidal streamwise gust is investigated using a multiple-fan actively controlled wind tunnel. The quality of the generated fluctuating flow was proved to be excellent (Yang et al 2017). The surface pressures of the airfoil are measured using DMS-4000 pressure scanners, and thus the lift force can be obtained by integration along the chord length of the airfoil.…”
Section: Introductionmentioning
confidence: 99%
“…The quality of the generated fluctuating flow was proved to be excellent (Yang et al. 2017). The surface pressures of the airfoil are measured using DMS-4000 pressure scanners, and thus the lift force can be obtained by integration along the chord length of the airfoil.…”
Section: Introductionmentioning
confidence: 99%
“…Ma et al (2013) determined the 2D AAF of the bridge deck in a wind tunnel, the multiple actively-controlled fans were used to simulate the streamwise velocity fluctuations, while the vibrating wings were used to produce the vertical velocity fluctuations. Later, Yang et al (2017) studied the 2D AAFs of a thin airfoil in experimentally generated sinusoidal flow with discrete frequency. Recently, with the help of active generation wind tunnels, an effective method is obtained to generate the downstream flow field (Wu et al, 2021).…”
Section: Article History Abstractmentioning
confidence: 99%
“…However, Yang et al. (2017) found considerable discrepancies between experimental results and Greenberg's prediction even under attached flow conditions. It should be noted that they experimentally chose a dimensionless gust amplitude of σ = 0.2, which is larger than that selected by Granlund et al.…”
Section: Introductionmentioning
confidence: 97%