The Interference Effects on an Airfoil of a Flat Plate at Mid-span Position (1931)
NASA Technical Reports Server (NTRS) · leaf 19
0 .2 .4 .6 g .8 1.0 1.2 1.4 ^ Fig.4 Airfoil-plate interference. Effect of fillets. Corrected to infinite aspect ratio. Average Reynolds Number = 3.6 x 106 1T.A.C.A. 0021
NASA Technical Reports Server (NTRS)
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