Maximum lift coefficient of symmetrical 10.51% thick airfoil was increased from 1.3 to approximately 1.8 by means of area suction from 0.3 to 3% chord.
Effect of type of porous surface and suction velocity distribution on characteristics of 10.5-percent-thick airfoil with area suction
NACA -- Tech Note
1953
59 pages
Report
Englisch
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