Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap
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"Effect of Reynolds Number on Aerody..." refers background or methods in this paper
...Based on the equation for optimum GF given by Traub and Agarwal [8], the optimum GF height varies from 2.7 to 4.2% of airfoil chord as Reynolds number decreases from 3.0 × 105 to 3.0 × 104....
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...[6], Brown and Filippone [7], and Traub and Agarwal [8] have studied the performance of airfoils at low Reynolds numbers but a systematic investigation is still not available....
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...Mueller and Batill [5], Selig et al. [6], Brown and Filippone [7], and Traub and Agarwal [8] have studied the performance of airfoils at low Reynolds numbers but a systematic investigation is still not available....
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...Based on the equation for optimum GF given by Traub and Agarwal [8], the optimum GF height varies from 2....
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"Effect of Reynolds Number on Aerody..." refers methods in this paper
...This is demonstrated by Arko and McQuilling [16], who used advanced turbulence models of Abe et al. [17, 18] and Kato and Launder [19]....
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...This is demonstrated by Arko and McQuilling [16], who used advanced turbulence models of Abe et al....
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