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High Advance-Ratio Airfoil Streamwise Oscillations: Wind Tunnel vs. Water Tunnel

机译:高进给比的翼型流向振荡:风洞与水洞

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NACA0012 and 0018 pitching airfoils in an oscillatory relative free-stream are examined in a water tunnel with an electric motion-rig to oscillate the test article, and in a wind tunnel with moving-louvers that vary flow speed in the test section, at reduced frequency k=0.074. History of lift and pitching-moment is compared between the two facilities and with the classical attached-flow theoretical treatment, for (1) combined pitch and free-stream oscillating, (2) pure pitch, and (3) free-stream oscillation at constant incidence. The pitch-motion takes the airfoil into and out of static stall, with consequent dynamic-stall effects, and departure from attached-flow theory on the downstroke. Relative streamwise oscillation at 50% of mean-value gives departure from quasi-steady lift, and also from attached-flow unsteady theories, depending on the phase of motion. However, coupling between the dynamic-stall from pitching and the relative free-stream oscillation is weak, suggesting that the two respective nonlinearities do not mutually couple. These broad trends were shown to be larger than discrepancy between wind-tunnel and water-tunnel results.
机译:用电动钻机在水隧道中检查振荡相对自由流中的NACA0012和0018俯仰翼型,以使测试物品振动,并在风洞中使用移动百叶窗改变测试部分中的流速,从而减小测试气流。频率k = 0.074。比较了两个设施之间的升力和俯仰力矩的历史,并使用经典的附加流理论处理,比较了(1)俯仰和自由流组合振荡,(2)纯俯仰和(3)在持续发生率。俯仰运动使机翼进入和退出静态失速,随之而来的是动态失速效应,并且偏离了下行冲程的附着流理论。在平均值的50%处,相对流向振荡会偏离准稳态升力,也可能会偏离附加流非稳态理论,这取决于运动的相位。但是,俯仰动态失速与相对自由流振荡之间的耦合很弱,这表明两个各自的非线性不会相互耦合。这些广泛的趋势显示出大于风洞和水洞结果之间的差异。

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