Inside Out Library

Report (1915)

United States. National Advisory Committee for Aeronautics, United States. National Aeronautics and Space Administration · Washington : G.P.O. · leaf 324

An illustration from Report, 1915, leaf 324
wtntwuci no. <»« -::.♦ p.j -.1 Angle of Attack In Degrees i VTf 10 \lil11 708090 1?§ 0.6 o.ol .08 3.07 .06 .05- .03 .02 0.6 B.ll-O.?! «.7|-i.i ■1^.7-i.y 18.H 1-J.C 6.0 --I i^ 12 Uo.i I^ 23.8 III -J.O REFEREBCE KO. *3 Percent of Chord70 60 -4 -2 RETEREHCE HO. ** … M. to. If.16l»1210 20 10 0 -10 0102030 Name of sectloa: Surasil Prop. 1^. Size of model: 18* x J*. Wind velocity: IW ft./see. Where tested: U.I.T. Date: 1918. Angle of Attack In Degrees Percent of Chord_U! &0 50 «0_ ~i—rtj—rt—in—rt—rt 6 40 u 50 S * P>G 70: •I80 ; »> 100?

Aeronautics

Internet Archive · Gerstein Library, University of Toronto · Public Domain Mark 1.0. Free to use for anything.

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