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Measurement of the True Dynamic and Static Pressures in Flight (1939)

NASA Technical Reports Server (NTRS) · leaf 31

An illustration from Measurement of the True Dynamic and Static Pressures in Flight, 1939, leaf 31
Figure 2.- Lines of equal flow speed according to computations from English wind tunnel measurements (ref. 4),

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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