Experiments with a Wing Model from which the Boundary Is Removed by Suction (1929)
NASA Technical Reports Server (NTRS) · leaf 39
N. A. C . A Figs.18,19 Tpchnical Meirorandum No.534 10 8 6 4 cm I— c 0 -2 ,06 .02 Fig. 18 Polar of thick strut v;ith different suction strengths is proportional to c^.l=10ci'n about. c. =1 cl … Fig.19 Characteristic curves of snail experimental blower in Section VIII. Notp.tion. u=i^'^r=peripheral velocity of im- pellers; p=difference between static pressure forward and aft of blower;v=velocity of flow through the annular section swept by ^impeller blades . y)=v/u=delivery coefficient; y…
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