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Aerodynamic theory and test of strut forms. Part I (1930)

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t stream and p, is in terms of po as a unit. Table II gives the values of ut, v„ q,, and pv derived from equations (3), (4), (5), and (6) for the United States Navy Number 2 strut. The values of the point pressure p, are shown plotted against the strut width in Figure 4 and against its half… … Figuse S.—Point pressure versus strut half thloJmessf or experiment and theory. The Joukowski and Rankine theoretical curves coincide

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