Pressure distribution over a Clark Y-H airfoil section with a split flap (1937)
NASA Technical Reports Server (NTRS) · 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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