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Flow phenomena on plates and airfoils of short span (1936)
NASA Technical Reports Server (NTRS) · leaf 34
N.A.C.A. Technical Memorandum No, 798 Tigs. 21,22,23,24 … the square plate at 30© J"igure 21.- Pressure angle of attack. distribution on the suction side of the square plate at 8° angle of attack. Figure 24.- Measured lift figure 23*- Experimental distribution and theoretical over the span of a normal-force distribution triangular plate, oyer the span of…NASA Technical Reports Server (NTRS)
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