Inside Out Library · Explore
The effect of small variations in profile of airfoils (1931)
NASA Technical Reports Server (NTRS) · leaf 18
W.A.O.A. Teclvnical Note No. 361 Fi N.A.C.A.-0021 N.A.C.A.-lOO Tjst No. -128 ^~ "Test No. 430 22 … 0 .2 .4 .6 ,8 1.0 1.2 Lift coefficient (absolute), 0^ Fig. 9 Oom-oarative curves for N.A.0,A.-0021 & N.A.C.A.-lOO R.N. = 3.4 X lO'^NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from The effect of small variations in profile of airfoils
More like this
