Effects of Propellers and of Vibration on the Extent of Laminar Flow on the NACA 27-212 Airfoil (1939)
NASA Technical Reports Server (NTRS) · leaf 10
N.A.C.A. F igs. 5,6 Position along span o 16 in. Jeff of center_ a At center □ /6 in. right of center_ Propeller removed \ CT= .068 … 10 20 30 40 50 70 60 Percent chord Figure 6. - Effect of 'ation on transition. 0 10 20 30 40 50 60 70 Percent chord
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
