Tests on airfoil sections in modified open-throat type wind tunnel developed for purpose of obtaining 2-dimensional airfoil data at transonic speeds.
Effect of thickness, camber, and thickness distribution on airfoil characteristics at mach numbers up to 1.0
NACA -- Tech Note
1956
75 pages
Report
Englisch
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Effect of Airfoil Thickness, Camber and Reynolds Number on Plunging Airfoil Propulsion
British Library Conference Proceedings | 2009
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