Measurement of the True Dynamic and Static Pressures in Flight (1939)
NASA Technical Reports Server (NTRS) · leaf 32
figs, 3,4 V.A.C.A. Technical Memorandum No. 913 … ^\Figure 4.- Lines of equal flow speed for a biplane according to computations by P. Ruden. \Hormal lift coefficient of the upper wing cno 0.50 cnu O-48 « « " " lower " Pioneer Instrument Co. (Prof. Go.Jd?) Lopres/e fr-ikf<k-t> von foumhouer^. mil Figure 3,- Lines of undisturbed flow speed for…
NASA Technical Reports Server (NTRS)
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