Data were obtained with model moving over water in towing tank through angle-of-attack range from -6° to 18° at heights of airfoil trailing edge above ground from 0.015 chord to 2 chords; effects of airfoil thickness and end plates were investigated.
Effect of ground proximity on aerodynamic characteristics of aspect-ratio-1 airfoils with and without end plates
NASA -- Tech Notes
1961
27 pages
Report
English
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Aerodynamic characteristics of several airfoils of low aspect ratio
Engineering Index Backfile | 1935
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