The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel (1932)
NASA Technical Reports Server (NTRS) · leaf 10
he Reynolds Number were increased. similar phenomenon in relation to the drag of spheres is discussed in reference 6.) The character of the Comparison of the scale effect in the different tunnels.—^The differences between the results from the discontinuity exhibited by the N. A. C. A. 102 airfoil… … -2 0 2-2 O 2 4 -2 0 2 4 6 -2 0 2 4 0 2 4 6 0 2 4 S 8 10 12 14 16 18. 20 22 24 26 oc u ex. a, ot cc Fianu 20.—N. A. C. A. 0031 aiifoQ. Results team, dosed-tliro&t tmmel showlnf sSect of inoreased turbnlenca estimate of the degree of the tmmel air-stream turbu- flow corresponding to the low-lift…
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