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Pressure distribution over a Clark Y-H airfoil section with a split flap (1937)

NASA Technical Reports Server (NTRS) · leaf 6

An illustration from Pressure distribution over a Clark Y-H airfoil section with a split flap, 1937, leaf 6
OLARK T-H AIRFOIL 8E0TX0B TiBLE I (Oxdinatee in percent of oboxd) L.X. Rad.: 1.50 … Figure 1.- OlarlE I-H sodel showing location of preeeure orifieea on airfoil and on split flap.

NASA Technical Reports Server (NTRS)

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