Aerodynamic theory and test of strut forms. Part I (1930)
NASA Technical Reports Server (NTRS) · leaf 6
m must be added to u, giving (5) for the resultant velocity of p. Then the pressure p, at p, above the stream pressure, is (6) where p0 is the dynamic pressure, £ pTJf, of the distant 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… … -1.00 Fiqubk t.—Curves of point pressure, pip, over surface ot Navy No. 2 strut from experiment and from Ranking and Jookowski theories sra and fe Figuse S.—Point pressure versus strut half thloJmessf or experiment and theory. The Joukowski and Rankine theoretical curves coincide
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