Inside Out Library · Explore

Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder (1927)

NASA Technical Reports Server (NTRS) · leaf 18

An illustration from Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder, 1927, leaf 18 — N.A.C.A. Technical MemoraniuiV; Fig. 6 CO a … > 1=1 <*: K -P CQ CD CD ?4 o o LO c LO o O LO LO •H -P fx, * CO in to CO CQ 05 H H o O

NASA Technical Reports Server (NTRS)

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

More pictures from Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder

More like this